calculations of flux spectra and energy deposition … · calculations of flux spectra and energy...
TRANSCRIPT
w
Atomic Energy of Canada. Limited
CALCULATIONS OF FLUX SPECTRA AND
ENERGY DEPOSITION FOR FAST NEUTRONS
by
K.K. MEHTA and P.R. KRY
WMt*th«ll NoeUor Research Esloblishm«n»
Pinawo, Manitoba
S«pt«mber 1969
ÂECU3423
> • 'I ' i i -
ATOMIC ENERGY OF CANADA LIMITED
CALCULATIONS OF FLUX SPECTRA AND
ENERGY DEPOSITION FOR FAST NEUTRONS
by
K.K, Mehta and P.R. Kry
Whitesheil Nuclear Research Kstabl i shmont
Pinawa, Manitoba
September 1969
CALCULATIONS OF FLUX SPECTRA AND
ENERGY DEPOSITION FOR FAST NEUTRONS
by
K.K. Mehta and P . R . Kry
AJBSTRACr
A FORTRAN IV code NEVEMOR has been written utilizing
a multigroup-multiregion method for calculating fast neutron flux
spectra, neutron energy deposition, and foil activations due to fast
neutrons in a heterogeneous lattice cell.
Estimates are made of the effects of using group cross
sections and of homogenizatiorw Non-isotropic elastic scattering of
neutrons off light nuclei (in the laboratory' co-ordinate system) is
considered by applying transport corrections in such cases. Inelastic
scattering is handled by assuming that there is only one state to which
the target nucleus could be excited, except for uranium-238 where detailed
group-to-group cross sections are used.
Values obtained with NEVEMOR for dose rates are compared
with earlier measurements in the WR-1 reactor at low-reactor powers.
The agreement is within 5%, The contribution to the close rates of the
neighbouring fuel cells is also calculated for WR-1. Rer.ults of experiments
in the NRX and NRU reactors also agree well with the values calculated
with NEVEMOR.
Whiteshell Nuclear Research Hstab 1 ishnuT.t
Pinawa, Manitoba
September 1969
AECL-3423
Calcul des spectres de flux et du dépôt énergétique
des neutrons rapides
par K.K. Mehta et P.R. Kry
Résumé
On a écrit NEVEMOR (code FORTRAN IV), en utilisantune méthode multigroupe-multirégion pour calculer les spectresde flux, les dépôts énergétiques et les' lames activantes deneutrons rapides dans une cellule de réseau hétérogène.
Des estimations sont faites en ce qui concerne leseffets de l'utilisation de sections efficaces de groupe etde l'homogénéisation. La diffusion élastique et non-isotropique des neutrons engendrés par des noyaux légers(dans le système de coordonnées du laboratoire) est considéréeen appliquant les corrections de transport employées dans detels cas. La diffusion inélastique est contrôlée en supposantqu'il n'y a.qu'un état auquel le noyau de cible peut êtreexcité, sauf dans le cas de l'uranium 238 pour lequel on utilisedes sections efficaces détaillées, de groupe à groupe.
Les valeurs obtenues avec NEVEMOR pour les débits dedose sont comparées à des mesures effectuées antérieurementdans le réacteur WR-1 a faible puissance. L'accord est de5% au maximum. La contribution aux débits de dose des cellulesde combustible avoisinantes est également calculée pour le WR-1.Les résultats d'expériences effectuées dans les réacteursNRU et NRX sont également en bon accord avec les valeurs calculéesgrâce a NEVEMOR.
L'Energie Atomique du Canada, Limitée
Etablissement de recherches nucléaires de Whiteshell
Pinawa, Manitoba
Septembre 1969
(i)
CONTENTS
Page
1. INTRODUCTION 1
2. THE METHOD 2
2.1 Outline of the Method 22.2 Flux Calculations 52.3 Energy Calculations 102.4 Foil Activations 16
3. USE OF THE PROGRAM NEVEMOR 17
3.1 Options 173.2 Material Identification 193.3 Input Data 213.4 Output 26
4. EFFECTS OF ZONE SIZE AND SCATTERING APPROXIMATIONS 27
4.1 The Effect on the Results of theNumber of Energy Groups 27
4.2 The Effect on the Results of theNumber of Regions 32
4.3 The Effect on the Results ofTransport Corrections 35
4.4 The Effect op. the Results of UsingAveraged Inelastic Scattering Cross Sections 38
5. APPLICATIONS 43
5.1 Whiteshell Reactor No. 1 (WR-1) 435.2 NRU Reactor 525.3 NRX Reactor 53
6 REFERENCES 54
APPENDIX 1 An Outline of Input Data and Available Options 57
APPENDIX 2 Explanation of Notations 60
APPENDIX 3 Normalization Factor ANORM 67
APPENDIX 4 Simplified Flow Chart of NEVEMOR 68
APPENDIX 5 Listing of NEVEMOR 70
APPENDIX 6 Sample Output from NEVEMOR 87
Cii)
FIGURES
Page
1, Comparison of Energy Flux Spectra for Two Cases:K = 51 Groups and K = 26 Groups (for centraldosimetry hole, 1 = 1 ) 28
2, Comparison of Energy Flux Spectra for Two Cases:K = 51 Groups and K = 26 Groups (for moderatorregion, I = 24) 29
3. Comparison of Integrated Flux vs Radius forThree Cases: N = 26, 14 and 9 Regions 33
4. Comparison of Integrated Flux vs Radius forTwo Cases: Forward Scattering Applied, andForward Scattering Not Applied 37
5, Comparison of Energy Flux Spectra for Two Cases:Group-to-Group Cross-Sections used for U-238,and Averaged Cross-Sections used for U-238 (forcentral dosimetry hole, 1 = 1 ) 40
6. Comparison of Energy Flux Spectra for Two Cases:Group-to-Group Cross-Sections used for U-238, andAveraged Cross-Sections used for U-238 (for fuelregion, I = 13) 41
7a. WR-1 Fuel Cell Geometry (stainless steel pressuretube, large calandria tube) 44
7b. WR-1 Fuel Cell Geometry (stainless steel pressuretube, large calandria tube) showing Annular^Regions used in NEVEMOR 45
8. Integrated Flux, Nickel Flux, and Energy Absorbedby Hydrogen vs Radius for WR-1 Fuel Site(stainless steel pressure tube, large calandriatube) 47
9a.. Fapt Neutron Energy Histograms for WR-1 FuelSite (stainless steel pressure tube, largecalandria tube) 48
9b. Fast Neutron Energy Spectra for WR-1 FuelSite (stainless steel pressure tube, largecalandria tube) 49
(iii)
TABLESj
Page
I Comparison of Energy Transferred to VariousMaterials in the Central Dosimetry Hole forK = 51 Groups and K = 26 Groups 30
II Comparison of Various Energy Values forK = 51 Groups and K = 26 Groups 31
III Comparison of Various Energy Values forN = 26, 14 and 9 Regions 34
IV Comparison of Various Quantities for TwoCases: Forward Scattering Applied andForward Scattering Not Applied 36
V Comparison of Energy Transferred to VariousMaterials in the Central Dosimetry Hole forTwo Cases: Group-to-Group Cross-Sections usedfor U-238, and Averaged Cross-Sections usedfor U-238 39
VI Comparison of Various Quantities for Two Cases:Group-to-Group Cross-Sections used for U-238,and Averaged Cross-Sections used for U-238 42
VII Various Energy Values for WR-1 Fuel Site 50
VIII Energy Transferred to Various Materials in theCentral Dosimetry Hole of WR-1 Fuel Site 51
- 1 -
1. INTRODUCTION
Radiation dosimetry is a very complex vet important subject
for many nuclear applications, and various computer programs have been
developed for its analysis. In this report, we explain and discuss the
code NEVEMOR developed during the dosimetry program at Whiteshell
Nuclear Research Establishment.
NEVEMOR is a Fortran IV, G-level computer program, developed
with the aim of computing various quantities related to fast neution
dosimetry in a heterogeneous nuclear reactor. In NEVF.MOR, one considers
a cylindrical lattice cell (a unit cell which repeats itself periodic^ ly
in space), and divides it into homogenized annular regions. The fast
neutron spectrum is then calculated for each region. From this, the
kinetic energy transferred from fast neutrons to each material in each
region is calculated. Radioactivity induced in various fast neutron
activation detectors can also be estimated. The dose rate and the
induced radioactivity can be measured experimentally, thus providing
a check on the calculations.
NEVEMOR is primarily an extension of an Apex language
program EPITHET ' , which uses a multigroup-multiregion method for
calculating flux spectra and neutron absorption at epithermal energies.
NEVEMOR incorporates two modifications applied to EPITHET *' . The first
of these extended the energy range from epithermal to fast neutrons
(0.1 to 10 MeV, for example) by including inelastic scat teri ig in the
calculations. The inelastic scattering reaction is treated as if there
were only one possible channel for such a collision in each energy group,
for each material except uranium-238. For U-23.S a full matrix of sroup-
to-group cross sections is read in. The second major modi(ivat ion was
the inclusion of corrections for forward scattering by light nuclei for
the flux calculations. For systems with uniform spatial distribution
of the sources of neutrons (e.g. fission), i\\i> im>ih i i i .n ion has c.encial 1\
a negligible effect. But, when the sources are cui: •'•nt rated in the inner
- 2 -
regions of the system, the forward scattering*corrections tend to flatten
the flux.
2. THE METHOD
2,1 OUTLINE OF THE METHOD
A cylindrical lattice cell is divided into N arbitrarily
spaced homogenized annular regions numbered from the innermost as 1
to the outermost as N, (N < 30). The neutron energy range considered
(from 10 MeV to some lower energy) is divided into (K-l) arbitrarily
spaced energy groups numbered from the highest as 2 to the lowest as
K, (K < 51), while the first energy group consists of all neutron
energies above 10 MeV. The basic unit for calculations concerning
this system is thus a zone, or the intersection of a group and a
region.
For the first energy group, a spatial flux distribution
is read in and normalized in the program to one source neutron in this
group over the whole cell.
For all other zones, the average neutron flux for each zone
is calculated from the total number of collisions, C. ,,* in that zone,1 ,K
working from the highest to the lowest energy; thus
The number of collisions in each zone is calculated from
the numbers of neutrons entering that zone and the cross sections for
the various reactions (elastic and inelastic scattering and neutron
* See Appendix 2 for explanation of the notations.,
- 3 -
absorption). Neutrons enter a zone from three sources: slowing-down
from higher energy groups in the same region, neutron currents from
adjacent regions, and source neutrons directly from fissions (or any
other source) in that zone.
The source neutrons are automatically given the same spatial
distribution as the flux in group 1, which is given as input data.
Their energy distribution is also given as input data. The neutron
currents from adjacent regions are calculated from conservation equations
involving probabilities of escape from or collision in a zone. Th°
slowing-down from higher groups takes place by two processes: elastic
scattering and inelastic scattering.
From the average neutron flux in each zone, the ki'.etic
energy transferred per second to each material in that zone is calculated
assuming only three types of reaction: elastic scattering, inelastic
scattering and neutron absorption. The total energy given off per
second as gamma rays in inelastic scattering reactions is calculated
by summing over the contribution from each zorc% The net energy flux
out of the lattice cell is calculated from the inward and outward
neutron currents at the cell boundary. The energy removed from the
system by neutrons slowing dowi. past the lower bound of the energy range
is also calculated. The distributed energy is totalled and then balanced
against the energy which is introduced into the svstem by source neutrons,
in order to check energy conservation. Foil activations are calculated
from the average neutron flux in a zone and the input differential
absorption cross sections for the foil.
The entire output is normalized by the factor .WORM* tc
any desired number of kilowatts of U-235 fission energy produced per
centimeter thickness of the lattice cell. The value of WORM depends
upon the fact that the source spectrum is normalized to one neutron
above 10 MeV over the entire lattice cell.
See Appendix 3.
- 4 -
The following assumptions and approximations are made
in NEVEMOR:
(i) The angular distr ibution of neutrons passing through
any surface is cosine-like. This assumption is
reasonable fer a medium whose absorption cross section
is small. Also, deviation from a cosine dis t r ibut ion
is associated with small currents and thus the effects
of such deviations are se l f - l imi t ing .
( i i ) Scattering-up of neutrons in energy is negl igible ,
( i i i ) Regions are homogeneous annuli.
(iv) The lower bound of the f i r s t group is 10 MeV. This
assumption pertains only to the normalization factor
ANORM.
(v) Neutrons in a given zone have a uniform d i s t r i b u t i o n
in space, and a 1/E spectrum in energy, the spectrum
being discont inuous at the group boundar ies . The l /£
spectrum i s a carry-over from the o r i g i n a l program
EPITHET, and i s adequate for p r e s e n t purposes . As
can be seen from the output s p e c t r a , * a 1/E spectrum
is a s a t i s f a c t o r y approximation above 3 MeV. Errors
due t o dev ia t ion from 1/E below t h i s energy a re small
s ince the energy involved i s sma l l e r and the energy
groups are also getting progressively smaller.
(vi) Nuclei have negligible kinetic energy prior to collision
with a neutron.
(vii) Elastic scattering is isotropic in the laboratory
system. At the user's option, however, corrections
for forward scattering by light nuclei for up to four
materials can be automatically applied in the program.
(D, H, C, 0 are the usual nuclei for which this option
is used.) 2 Inelastic scattering, which is important
only for heavy nuclei, is isotropic in the laboratory
system.
* See Section 5.
- 5 -
(viii) There is no inelastic scattering in croup l.
(ix) For all materials except uranium-2:J8, a nucleus can
be excited to only one energy state by a neutron in
a given group. This excited state is taken as a
weighted average cf all possible states. (Alternatively,
one could choose any isotope in placp of U-238 if
necessary cross section data are provided.)
(x) For U-238, the excited states of the nucleus are not
considered directly, but rather group-to-group in-
elastic scattering cross sections arc read in.
(xi) For inelastic scattering calculations, all neutrons
in a group have the average neutron energy of that
group.
(xii) If an absorption takes place the energy transferred
as kinetic energy to the nucleus is just the energy
associated with the motion of the center of mass.
The remainder of the neutron's energy does not contri-
bute to the recoil energy of the nucleus, but eventually
appears as radiation (e.,g., gamma-ray) energy,
2.2 FLUX CALCULATIONS*
The total number of collisions in a zone is the sum of
three terras: the number of neutrons entering the ^one by slowing
down in the same 1 ion (this includes source neutrons), the number
entering through the inner surface of the region, and the number
entering through the outer surface of the region, multiplied by the
respective probabilities of collision for a neutron which enters by
one of these three methods. Hence,
* See Appendix 2 for explanation of the notations.
- 6 -
The inward and outward neutron currents (J. . , and J, ,.) from
the zone (i,k) satisfy the neutron conservation relations, viz.,
and
*J i K = Qi h W| i, + J|-l,k wi,k "*" J i,k "I,»
[2-21
+ d,o - 0,0 r .,
The calculation of the neutron currents from these equations and the
calculation of the nine probabilities (W's) are described in detail in
Reference 1.
In NEVEMOR, Q. , is made up of three terms: elastic andl ,K
inelastic scattering contributions, and a contribution from source
neutrons. The elastic scattering contribution is described in detail
in Reference 1. The number of source neutrons in each group is input
data, which is normalized to 1 neutron above 10 MeV over the whole cell,
and is given the same spatial distribution as the input flux shape for
group 1.
Inelastic scattering is handled by two methods in NEVEMOR.
For U-238, a group-to-group inelastic scattering cross section matrix
is read in. Thus if a?, , is the inelastic scattering cross section
from group k1 to group k, and if K (K ^ K) is the last and the lowestin ID
group for which inelastic scattering cross section data are considered,
the following matrix is read in:
- 7 -
or3,3 3,4
• •
K
These cross sections must be normalized, so that
Kro . Tz. a- - a;h=k! k > it»
the to ta l inelast ic scattering cross section for group k ' . The number
of neutrons slowing down into group k from group k' due to inelastic
scat tering collisions with U-238 is
The second method of dealing with inelast ic scattering is
applicable to a l l materials . The average neutron energy, E, , , in group
k ' , i s defined by
•/En'EdE
E
dEE
loge
L ~ E k '
EK'-1EK"
E L . = = {2mS]
IVhen a neutron of a given energy excites a nucleus in an inelastic
scat ter ing reaction, there are usually several gamma rays the nucleus
might emit. If EY, EY, . . . EY are the energies of the gamma rays1 2 M
- 8 -
which could be emitted, then associated with these are the cross sectionsT T T
a , a , . . . a , for the given incident neutron energy. Thus, for every1 2 m
material, the input data comprise a cross section and a weighted, gamma-
ray energy for each neutron energy group. The cross section used for
a material j and group k1 is
The gamma-ray energy used is the average gamma-ray energy with which
the nucleus decays, i.e.,
r
For U-238, which has the group-to-group cross section matrix,
values of a. ,. are also read in. This is a total cross section for
group k1 neutrons to scatter inelastically to any lower group, even below
group K . To consider inelastic scattering for U-238 across the lowerm j
energy bound K , the program reassigns a new value to a. . ,, viz.,
The second term in the above expression is the sum of all the elements
in (k'-l) row of the matrix, i.e., it is the cross section for group
k' neutrons to" inelasticaliy scatter to any lower group above group
K . Also, all of the available neutron energy (excluding center-of-
mass energy) is assigned to EÏ .,. The assignment is done, because
for all but the lowest energy groups
I Km :
and for the lowest energy groups, if an inelastic scattering reaction
occurs, practically all of the neutron energy is converted into gamma-
ray energy.
If E^, is the initial neutron energy of a group k1 neutron,
- 9 -
its final energy after an inelastic scattering collision with a nucleus
of atonic mass A. will be*J Z
I—i A IE" •" JT^W ^ - -TT7 EJ>
12-61
The neutron is then assu d to end up in group k, if
i—i
Since a l l neutrons which undergo i n e l a s t i c s c a t t e r i n g in a group are
assumed to have the average group energy, the number of neutrons slowing
down into group k from group k ' , if condition 2.7 holds, is
4>i.*' Vi [2.8]
and I. . , = 0 if condition 2.7 does not hold.
Adding all of these contributions together gives
where q. . , , is the number of neutrons elastically scattered into
group k from group k' by the j material in region i.
An important quantity in the calculation of the nine
probabilities is the probability of production of a secondary neutron
in each zone, or, in other words, the number of neutrons in zone (i,!O
which have come from collisions in that zone divided by_ the total collisions
in that zone. The calculation of the number of inelastic scattering
reactions which result in secondary neutrons depends on the method of
handling inelastic scattering. For U-238, the number of secondary
neutrons is proportional to
\ ' (Ek-l/Ek >
See Section 2.3, equation 3.5
- 10 -
For all other materials, ET , ïs significantly greater than a typical
energy group width, so that it is assumed there is no contribution to
secondary neutrons from this method of dealing with inelastic scattering.
Also, as in Reference 1, let the number of elastic scattering collisions
which result in secondary neutrons in zone (i,k) be proportional to
N? . ,. Now, the total number of reactions or collisions with material
j in zone (i,k) is proportional to
Hence, the probability of production of a secondary neutron in zone
(i,k) is 9 j
[2.10]
As part of the optional output of NEVEMOR, one can calculate
a neutron flux energy spectrum averaged over the entire cell. This
average is weighted by the amount of a given material in each regjonsand thus the flux spectrum one calculates is the average flux spectrum
seen by the material in the entire lattice cell. Hence,
[2.11]2. Nj j Vj
2.3 ENERGY CALCULATIONS
Using the notation described in Appendix 2, the equations
governing scattering reactions' are as follows:
Conservation of Energy;
V E c s En +Ej = En + Ej + E 7
- 11 -
where EY = 0 for e last ic scat tering.
Conservation of Momentum;
EJ "" E ) » / A [3.21
and since *E. i s assumed to be zero ,
E c = ' E n / ( A + 1 ) [3.3]
Using the cosine law to transform to the laboratory systenr3 ,/ • v 1 ^
• El - 2ACoSflV. ElI A+l I
If the scattering is isotropic in the center-of-mass system, the averaget t
value of E. is• zir rzir
•E; <e / JI
A+l ' y[3.4]gA('En) I" (At-1) J _ 1
(A+l)2 L 2 A 'EnJ
where equations 3.1, 3.2 and 3.3 have been used.
The second energy of interest in a scattering reactioni i
is E . Using the cosine law to transform to the laboratory system,
•=• [ A2 + 1 "I . A2 + 1 "I .+1)Z J E'
and as before, if the scattering is isotropic in the center-of-massgsystem, the average value of En is
(4^) 13.51
- 12 -
In the case of inelastic scattering off U-238, the final
neutron enerpy is taken as the average energy of the group it scatters
into, i . e . ,
n k n k
if the neutron scatters from group k to group k'. The energy transferred
to the j material in region i by a group k neutron which inelastically
scatters to group k1 is given by
Using equation 3.5, which must be satisfied by Ë, , Ë., » and
i—i
For an absorption reaction, it is assumed that only the
center-of-mass energy appears as kinetic energy of the nucleus, the
remainder of the neutron's initial energy being converted into radiation
energy'. Thus, for an absorption reaction in group k, the energy
transferred to the j material is
- £ - * k [3.73
where equation 3.3 has been used. The energy A.ÏÏ,/(Aj + 1) is classed
under the heading "non-center-of-mass energy in absorption reactions."
The total energy transferred per second to the j material
in region i by group k neutrons is
Summation over k gives the kinetic energy transferred per second to the
j material in the i region.
- 13 -
The total non-center-of-mass energy lost every secondin absorption reactions is
[3.9]
The total neutron energy converted to gamma-ray energy
every second by inelastic scattering is
i,jfk L '»k • i»J Ji^ i»'* •»J<
Here, the contribution, F. . . , made by U-23n is expressed as1 >3 t*
V N „' .e y ,1ui k.k j,k,k
where E! . , , is calculated using equation 3.5.
One other calculation is made concerning slowing-down,
and that is the energy per second which is taken out of the system by
neutrons slowing down past the lower energy bound of the system. As
the group-to-group inelastic scattering cross sections do not extend
below the lowest energy group, this method of dealing with inelastic
scattering does not consider any neutrons slowing down past the lower
energy bound. However, the other method calculates the average
neutron energy after an inelastic scattering reaction in zone (i,k)
and if this is below the energy range, then this energy is considered
lost to the system.. Therefore, the energy lost to the system by this
type of reaction is
= S itkN
I• *J
if 'E' < E,, where equation 3.5 is used to calculate E .
Neutrons also slow down past the lower energy bound of
the system due to elastic scattering collisions. The average energy
loss per second due to neutrons in group 1 slowing down past the lower
energy bound (E..) due to such collisions with the j material in zone
(i,D is
13.10]
[3.11]
[3.12]
- 14 -
:;, -s: dE
(for E, < EK tec. )1 K j
since h(Ev + a.E) is the average final energy with which such neutronsK jleave the system. Integrating,
\ i EKilEK
if Ex
and , , , = o >f Ei > —r
The calculation of the average energy loss per second due to neutrons
in group k (upper energy bound E, A, lower energy bound E,) slowing
down past the lower energy bound of the system by means of elast ic
collisions with the j material in region i , must be broken up into
two cases:
Case I
»-l >
i.j.k
t. N . a. ,.
V. N• i»)
2(1- « ) log (Ej • '
Ek+ a. E
JL + « : * - 2 * !k LK
dE
E
[3.13]
[3.14]
Case II
N
i - l
1 V F log (E. /E
i i l2 ( 1 - ^ )loge
EK~
(1-oME
K
X _ _ L \ - « 2 ( E ,Ek W J M
dEE
[3.15]
- 15 -
As can be seen from Table VII (page 50), the total energy
lost due to neutrons slowing down past the lower energy bound of the
system amounts to about 3% of the total input energy. This energy
could be distributed over various materials according to their mass
number and their macroscopic elastic cross section, say, at 0.1 MeV.
There is one other energy loss to the system and this
is the loss due to neutron leakage from the outer boundary of the
lattice cell. The gross energy fluxes into and out of the cell due to
group k neutron currents are:
" JN,k
The difference between these two fluxes gives the net energy flux
out of the cell every second.
The final distribution of neutron energy is then checked
against the total energy introduced into the system each second by
source neutrons.
For all groups but the first, the energy introduced per
second by source neutrons is S.E . The energy introduced into the
system by group 1 neutrons is calculated by replacing E,, by Ej in
equation 3.13 as this would then give the average energy of the neutrons
which have slowed down past the upper bound of the energy range. Thus,
is the average energy introduced into the system by group 1 neutrons.
- 16 -
2,4 FOIL ACTIVATIONS
Foil activations are calculated quite readily in NEVEMOR
because the neutron flux spectrum in each region is available.
Thus, i f
A ^ A&. . =rr p F- & * log U 4- 2 (A. 0"- . [4.1]
I,J — i j ,1 e ^,2 n f k j , k
then (a. . 10~21*) is the number of atoms activated per foil atom present
per second of irradiation time, where 4> is in cm 2 sec 1 and a is in
barns. \i£\ is the highest energy for which group 1 absorption reactions
are considered. Converting this to disintegrations per second per
milligram of sample per minute of irradiation, the activation becomes
•2* v x 10*3x 6.023 x 10
* (0.025)AT
when the irradiation time is short compared to the half-life of the product
nucleus. Here v is the isotopic abundance, A is the atomic mass of the
foil material atoms, and T is the half-life of the activated isotope.
The activation is also expressed in terms of an effective
flux, <ï>, or more precisely, a fission-spectrum integral flux. ^ If
a is the mean activation cross section for neutrons possessing a Cranberg
prompt fission-neutron energy spectrum, then
- " * ' • ' [4.31
Thus, 4> is calculated from a. . and an input value for a.1 » J
- 17 -
3. USE OF THE PROGRAM NEVEMOR
3.1 OPTIONS
Each problem run in NEVEMOR is controlled by the first
card in the data deck, which contains 40 two-digit integer variables,
forming an array called OPTION. Appendix 1 briefly summarizes what
will be discussed in this section, namely, what each of these 40
variables does.
QPTION(l) controls the input of data for each problem.
A 0 terminates the program. A 1 causes the energy data to be bypassed
so that only the geometry data mujt be read into the program (and possibly
the activation foil data). A 2 reverses this situation by causing the
geometry data to be bypassed, A 3 causes the program to read in both
energy and geometry data. A 4 causes the program to bypass reading
these data, ai well as all the calculations. This last option is
useful because one must specify all the output one wants, which is
impossible with just 40 options. Thus in effect, this option, allows
one to obtain more outputs.
OPTION(2) controls the corrections for forward scattering
by light nuclei. If it is 1 the transport corrections are applied.
If it is 0, they are not.
OPTION(3) controls the output of the data used in the
problem. A 0 suppresses this output; a 1 causes only-the geometry data
to be printed out; a 2 causes only the energy data to be printed out;
while a 3 causes all the data to be printed out.
OPTION(4)9 if 1, causes the program to read in a spatial
neutron flux distribution for group 1, while if 0 causes this distribution
to be automatically set uniform over the whole cell.
OPTION(5) controls the calculated neutron flux output.
- 18 -
A 0 suppresses it. A 1 suppresses the output of neutron flux energy
spectra. A 2 causes neutron flux spectra (per unit energy) to be printed
out for at most six regions. A 3 causes neutron flux spectra (per unit
lethargy) to be printed out for at most six regions. A 4 causes both
types of spectra to be printed out for at most six regions.
OPTION(6) to OPTION(11) specify the regions for which
the flux spectra of OPTION(5) are printed out.
If OPTION(12) is 0, the integrated neutron flux in each
region is not calculated, but if it is 1, this flux is calculated and
printed out as a function of radius.
OPTION(13) to OPTION(15) specify the reference numbers of
those materials for which the weighted average of the neutron flux
spectrum over the cell is calculated and printed out.
OPTION(16), if equal to 1, causes the total energy transferred
to the materials in the lattice cell to be compared with the energy losses
from the system. A 0 suppresses this output.
OPTION(17), if 1, causes the final distribution of neutron
energy to be compared with the initial input energy. A 0 suppresses
this comparison. This option checks energy conservation in the system.
OPTION(18) to OPTION(23) specify the regions for which
the energy transferred per second and the energy transferred per gram
per second are printed out for each material in the region.
OPTION(24) to OPTION(27) specify the reference numbers of
the materials for which the total energy transferred per second through-
out the whole cell is calculated and printed out.
OPTION(28) and OPTION(29) specify the numbers of two regions
which define the boundaries of an annular portion of the lattice cell
for which the total neutron energy transferred per second to all materials
is calculated. The two regions are included in this portion.
If OPTION(30) is 0, the program automatically starts a new
problem so that the activation foil data are not required as input.
- 19 -
When this option is non-zero, its value, Nlf is the number of regions
in which the first foil material appears, (N'^9). The next N] options
then specify these regions. OPTION (SHNj), if 0, sends the program to
a new problem, or specifies the number of regions, N2, the second foil
material appears in, (N^S-Ni). This sequence continues to OPTION(39),
which must either be the last region to contain the last foil material,
or be 0.
OPTION(40) suppresses the output of foil cross sections
if it is 0, and causes this print-out if 1.
3.2 MATERIAL IDENTIFICATION
Up to twenty materials can be handled by NEVEMOR. Each
material is arbitrarily assigned a two-digit number between 1 and
20 inclusive, and all data pertaining to this material are referenced
by this number. MPJ* is a reference number of an activation foil
material, and is non-zero only if it is also a reactor material, in
which case MPJ is equal to the reference number of that material.
The inclusion of a preceding digit enables one to determine
how the material shall be handled in the calculations. This three-digit
identification number is the one read in as MRC(I,J). Thus, the first
digit indicates how to treat the material, and the last two give the
reference number for all pertinent data for that material.
There are four choices for the first digit of a material
identification number. A 0 indicates that the material is to be treated
as a normal constituent of the reactor affecting slowing-down of neutrons
and absorbing fast-neutron energy. A 1 indicates that the material does
not affect eleastic scattering, but that it does absorb energy. This
option is useful for small numbers of heavy atoms for which inelastic
scattering is more important than elastic scattering. Some computing
* See Section 3.3.D
- 20 -
time is saved by use of this option. A 2 indicates that the material
does not contribute to s lowing-dovm of neutrons, but it does absorb energy.
This option saves computing time, but eliminates the usefulness of
energy conservation as a check on the calculations. The option is useful
for calculating the energy transferred per gram to small amounts of a
given material, in different parts of the lattice cell. A 3 indicates
that the material is to be treated as a normal constituent of the reactor,
but in addition the inelastic scattering matrix of group-to-group cross
sections has been assigned to this material. The reference number of
this material must be equal to IMAT.
The full complement of 20 materials can only be used if
one does not use the option of correcting for forward scattering by
light nuclei. This correction introduces 4 new materials which occupy
the reference numbers 17, 18, 19, and 20, corresponding to the materials
occupying the reference numbers 8, 9, 10, and 11, respectively. As
explained in Reference 2, these new materials affect only the spatial
scattering, and not the slowing-down calculation, of the materials that
they are related to. For example, if one wishes to correct for forward
scattering by hydrogen, one could assign its reference number to be 9
and the program would then set up a fictitious material with reference
number 18, which would affect only the assumed isotropic elastic scattering
enough to correct, for the forward scattering by hydrogen nuclei. Therefore,
if one wants to correct for forward scattering by light nuclei for up
to four materials, one assigns these materials the identification numbers
008, 009, 010 and/or Oil; and then one takes the option of including
transport corrections.* One must not, then, assign any data to reference
numbers 17 through 20, as these will be occupied by the new materials.
In other words, NMAT < 16 if transport corrections are applied.
* See Section 3.1.
i l -
3.3 INPUT DATA*
The input data required by NEVEMOR consist of 4 sets
of data cards: Options, Energy, Geometry, and Activation
Foil Detector.
A. The "Option" section consists of one card and contains
40 variables which control the program as mentioned
earlier. Its description is as follows:
OPTION (I) (1 = 1,40)12
fl. ENERGY DATA
This section requires OPTION(1) to be set equal to
2 or 3. The first card contains an arbitrary description
of the energy data, e.g., "51 GROUP HNERGY DATA FOR
NINE MATERIALS INCLUDING INELASTIC MATRIX FOR U-238".
Subsequent cards contain information as to the number
of energy groups, energy bounds of these groups, and
the source spectrum which enters the system. It also
contains cross sections for various reactions of neutrons
with all the reactor materials of interest as well as
gamma-ray energies associated with inelastic scattering
and their respective probabilities. The description
and the list of data cards for this section are as
follows :
(i) TITE(I) (1=1,20)A4
This section contains an arbitrary alphameric description
of the data.
( i i ) EL(1), VK(1), KLM, KIN, IMAT, NMAT, NSOPF10.5 F9.7 13 13 13 13 13
* See Appendix 1 for an outline of this section.
- 22 -
EL(1) is the lower bound of group l, (MeV).
VK(1) is the width of group 1 for absorptions,
i.e., absorptions are considered to take
place only up to a neutron energy of
VK(1)EL(1). VK(1) = 1 is allowed.
KLM is the number of energy groups used,
(KLM<60).
KIN is the lowest and the last group for which
group-to-group inelastic scattering cross
sections are given (O^KIN^KLM).
IMAT is the two-digit reference number for the
material which is to be assigned the group-
to-group inelastic scattering cross sections.*
NMAT is the number of materials for which cross
section data are to be given, (NMAT,.<20) .*
NSOR is the number of energy groups which
virgin fission neutrons or source neutrons
enter, (QsNSORsJCLM).
(iii) EL(K) (K=2,KLM)F10.5
EL(K") is the lower energy bound of group K, (MeV).
(iv) Cross section data for materials . This section
is repeated NMAT times.
(SUBST(MPR(M),L),L=1,4), MPR(Mj), AMASS(MPR(M))A4 12 F8.4
SIGA(MPR(M),K) (K=1,KLM)F10.5
SIGE(MPRO0,K) (K=1,KLM)F10.5
SIGI(MPR(M),K) (K=1,KLM)F10.5
EGAMACMPRCM^K) (tel.KLM)F10.5
* See Section 3.2.
SUBST(MPR(M),L) is an arbitrary alphameric
description of the material, (usually i t s
name),
MPR(M) is a two-digit reference number for tiie
material.*
AMASS(MPR(M)) is the atomic mass of the nuclei of
the material, (in units of neutron mass]»
SIGA(MPR(M),K) is the differential absorption cross
section of the material, (barns).
SIGE(MPR(M),K) is the differential elastic scattering
cross section of the material, (barns).
SIGI(MPR(M),K) is the differential inelastic scattering
cross section of the material as described in
Section 2.2,(barns).
EGAMA(MPR(M),K) is the gamma-ray energy associated
with inelastic scattering of group K neutrons
as described in Section 2.2, (MeV).
Each subsection starts on a new card.
(v) This section requires NSOR > 0o
SOURCE(K) (K=1,NSOR)F10.5
SOURCE(K) i s the number of source neutrons en te r ing
the system in group K,
(v i ) This s e c t i o n r equ i re s KIN > 2.
SIGIN(I) . ( I = l , KIN(KIN-l)/2)F10.5
The a r ray SIGIN** i s the mat r ix of group- to-group
ine l a s t i c scat ter ing cross sections in the order:
a , fl , a , . . . . o - ' „ , rr , a-1 , . . . .2»2 2>3 2,k 2 ' m * ' 3 3 j L |
3' m •*"• 4'Km m m
* See Section 3.2.
** See Section 2.2 and Appendix 2 for notations.
- 24 -
C. GEOMETRY DATA
This s e c t i o n requires OPTION(1) t o be s e t equal
to 1 or 3. The f i r s t card contains an arbi t rary
description of the geometry data, e .g . , "TRANSPORT
CORRECTION APPLIED TO WR-1 GEOMETRY". This section
contains information regarding the number of
annular regions, boundary condition and normalizing
reactor power density. It also l i s t s the outer
radii of a l l the regions, the atomic, densit ies
and the identif icat ion numbers of all the materials
in various regions, and the spat ia l dis tr ibut ion
of input neutron flux. The description and the
l i s t of data cards far this section are as follows:
(i) TITG(I) (1=1,20)
A4
This section contains an arbitrary alphameric
description of the data.
( i i ) N, COJ ENORM
13 F8.6 E14.7
N is the number of annular regions, (O^N^SO).
COJ is the albedo at the boundary of the
la t t ice c e l l , (if COJ<0.001, COJ i 1.)
ENORM is the number of kilowatts of U-235
fission energy produced per centimeter
thickness of the l a t t i ce c e l l . All outputs
are normalized to this number.( i i i ) JL(I) (1=1,N)
13
JL(I) is the number of materials in region I.
If JL(I)>100, then region I has the same
materials and atomic densities as region
(JL(I)-IOO).
- 25 -
(iv) R(I) (1=1,N)F7.4
R(IJ is the outer radius of region I, icmj,
(v) This section is repeated for all regions (I=1,N).
MRC(IfJ), DENS(I,J) (J=1,JL(I))13 F11.9
MRC(I,J) i s t h e t h r e e - d i g i t i d e n t i f i c a t i o n number
of t he J ' m a t e r i a l in reg ion ' , *
DENS(I,J) i s the atomic d e n s i t y of t h i s m a t e r i a l
in reg ion I .
( v i ) T h i s s e c t i o n r e q u i r e s OPTION!4) = 1.
FIN ( I ) (1 = 1,MF7.4
FIN ( I ) i s the neu t ron flux above 10 MeV in region 1
D. ACTIVATION FOIL DATA
This s e c t i o n r e q u i r e s OPTION! M)} t o have a non-nero
v a l u e , and con t a in s i n f o n n a t i o n r e g a r d i n g
a l l t h e f o i l d e t e c t o r s t o be p laced w i t h i n the
r e a c t o r l a t t i c e c e l l . I t c o n s i s t s of t he names and
t h e r e f e r e n c e numbers of the f o i l m a t e r i a l s , t h e i r
n e u t r o n a b s o r p t i o n c r o s s s e c t i o n s , h a l f - l i v e s of
t h e a c t i v a t e d i s o t o p e s , e t c . The d e s c r i p t i o n and
t h e l i s t of da t a ca rds fo r t h i s s e c t i o n a r e as
f o l l o w s :
( i ) ( A L P ( I ) , I = 1 , 9 ) , MPJ, CROSS, TAU, A, AI.
A 4 1 2 F i l ) . S H 1 4 . 7 F 9 . S F 9 . " 7
ALP(I) i s an a rb i t r a ry alphameric descr ip t ion of
the foil ma te r i a l .
MPJ i s the two-digit reference number of the
fo i l ma te r i a l .*
CROSS is the mean absorption cross sec t ion of
the material for neutrons poss- '^iny. a
* See Section 3.2.
- 26 -
Cranberg prompt fission-neutron energy
spectrum, [barns).
TAU is the ha l f - l i fe of the activated species,
(seconds).
A is the atomic mass of the foi l material.
AL is the fractional isotopic abundance,
( i i ) This section requires MPJ=0.
SIGAF(K) (K=1,KLM)F10.5SIGAF(K) is the differential neutron absorption
cross section for the foil material.
Up to five different foil materials can be treated by
NEVEMOR. Sections (i) and (ii) are then repeated the corresponding
number of times.
3.4 OUTPUT
The output of NEVEMOR is very flexible, thus, any or all
the quantities, e.g., fluxes, spectra, energy transferred,
calculated by the program can be output. The choices are
made by the use of the option section. In addition, any
input data can also be output. Following is the list of
possible outputs:
(i) flux spectra (per unit energy and/or unit lethargy)
for at least six regions
(ii) integrated flux (over the entire energy range) vs.
radius
(iii) weighted flux spectra for at least four materials
(iv) total energy transferred to all the materials in
the entire cell
(v) energy flowing out of the cell boundary
(vi) total energy lost due to neutrons slowing down past
the lowest energy bound of the system
(vii) total energy input into the system dut- to source
neutrons
(viii) energy converted intc gamma-ray energy associated
with inelastic scattering
fix) non-center-of-mass* energy in absorption reactions
(x) energy per gram transferred and energy transferred tc
each material for at least six regions
(xi) total energy transferred to at least four materials
(for the entire eel 1)
(xii) total energy transferred within an annulus defined
by two regions
(xi i i activities and effective flux for at least five foil
detectors in various regions
(xiv) any energy, geometry,- or activation foil input data
4. EFFECTS OF ZONK SIZF. AVO SG\TTliRl\G APPROXIMATIONS
4.1 TIE EFFECT!' ON Till: RESULTS 0l: Till. NUMHLU Oi: HNT.RGY URiDPS
Since group cross sections are used in \TVHMOR, there
are always present inherent errors in the calculated values of various
quantities. By increasing the number of groups, and thus decreasing
the size of each group, indefinitely, these errors can be made very
small. However, in practice, the computer time and the computer memory
needed limit this process. The choice of 60 groups in NHVMMOK is a
compromise between these situations.
To estimate the errors due to a finite number of energy
groups (K), two computer runs were made using IVh 11 es!uj 1Î Reactor No. 1
* See Section 2.3.
- 28 -
(A*M xn~U
V)
Il
o
o
»
«24-1O
I-H
X O3 X
Où O
u eV -Hw o-a
CO C
0J
8OU
3
84
10
zoX
10'"-
51 GROUPS
26 GROUPS
ID
NEUTRON ENERGY (M«V)
10
FIGURE 2: Coraparison of Energy Flux Spectra for Two Cases: K - 51 Groups and K = 26 Groups(for moderator region, I -- 24)
- 30 -
TABLE I
.COMPARISON OF
ENERGY TRANSFERRED TO VARIOUS MATERIALS* IN THE CENTRAL DOSIMETRY HOLE
FOR K = 51 GROUPS AND K = 26 GROUPS
Mate r i a l
Hydrogen
Deuterium
Carbon
Oxygen
Aluminum
Iron
Zirconium
Uranium-235
Uranium-238
51 Energy Groups 26 Energy Groups
2.569+
0.884
0.0398
0.0242
0.00829
0.00208
0.00127
0.000216
0.000227
2.571
0.886
0.0397
0.0244
0.00830
0.00209
0.00127
0.000217
6.000227
Difference (%)
+0
+0
-0
+0
+0
+0
0
+0
0
.08
.23
.25
.83
.12
.48
.46
Negligible amounts of various materials were placed in the central
hole (which is empty otherwise) to calculate the energy transferred.
+ All energies given in watts/gram.
- 51 -
TABLE II
COMPARISON OF VARIOUS ENERGY VALUES FOR K = 51 GROUPS AND K = 26 GROUPS
51 Energy Groups 26 Energy Groups Difference
Outward energy flowthrough ce l l boundary'
Energy lost throughlower energy bound
Energy t rans fe r red t omaterials in the entire cell:
HydrogenCarbonU-235U-238
Energy transferred tomaterials outside pressuretube
Computer memory' used
Computer time
8.839t
0.759
16.950
106K
65.17sec
8.921
0.758
17.047
88K
50.69sec
+0.93
-0.13
2.1430.5050.001100.0485
2.1450.5050.00110 .0.0486
+ 0.0900
+ 0.21
+ 0.57
+ All energies given in watts.
- 32 -
(WR-1) geometry data;* one with K = 51, another with K = 26. Except
for group 1, the groups in the latter case were made up by merging two
adjacent groups of the first case. Averaged inelastic cross sections,
instead of group-to-group matrix, are used for U-238 for both the cases.
Output energy spectra for these two cases are compared
in Figures 1 and 2 for two spatial regions. It can be seen from these
that the spectra are very similar for the two cases. It can also be
seen from Tables I and II that all the calculated energy values are the
same within less than one percent.
Thus, it can be concluded, at least for WR--1 geometry,
that for the case of K = 51, the error introduced due to finiteness
of the energy groups is negligible. Alternatively, hardly any advantage
can be gained by increasing the numbers of energy groups to more than
SI.
4.2 THE EFFECT ON TIE RESULTS OF THE NUMBER OF REGIONS
Since NEVEMOR homogenizes each region, inherent errors
in the calculated values of the various quancities are unavoidable.
The magnitude of these errors will depend upon the geometry of the
system and also upon the number of spatial regions the system is divided
into. There may exist an optimum region dimension as suggested by
Askew 5 . The program at present uses a maximum of 30 regions.
To estimate the effects of the number of regions (N),
three computer runs were made using WR-1 geometry data*, with N = 26,
14 and 9 (the number of fuel regions was 8, 4 and 2, respectively).
In all the cases, the region boundaries were the natural boundaries
dictated by the geometry of the fuel channel. The group-to-group
inelastic cross section matrix is used for 0-238 for all the cases.
* See Appendix 6 for geometry data.
- 33 -
,13
(M
eu• s .
cX_lIL
ZOCEh-
UJ
Z
r
—OCD• • •
I
T 1
i i
"1 1 1 1—
\
I i i 1
1
O
•
T
IM -
N -
H'-
\
1
! •
14
9
1
!
•
1
T
-
10 12
RADIUS (cm)
FIGURE 3: Comparison of Integrated Flux vs Radius for Three CasesN = 26, 14 and 9 Regions
- 34 -
TABLE I I I
COMPARISON OF VARIOUS ENERGY VALUES FOR N 26, 14 AND 9 REGIONS
Total energy transferred(watts]
Energy transferred to materialsin central hole (watts/gram)
N = 26
20.388
N = 1 4
20.440
Total energy transferred(watts)
N = 9
20.610
HydrogenDeuteriumCarbonOxygenAluminumIronZirconiumUranium-235Uranium-238
2.5550.8820.03950.02440.008260.002070.001260.0002160.000226
2,4440.8470.03790.02340.007920.001990.001200.0002070.000217
2.2690.7870.03520.02170.007360.001850.001120.0001920.000201
HydrogenCarbonU-235U-238
2.13200.50250.001090.0484
2.12350.50220.001060,0470
2.1760.51640.001010.0444
Energy transferred tomaterials outsidepressure tube
16.942 17.025 17.172
Various outputs are presented in Table I I I .
The to ta l energy transferred to materials in the cell is about the
same for a l l the cases. (This i s because albedo a = 1.) As can be
seen from Figure 3, the integrated flux in the central hole is
decreasing as the mesh gets coarser, and this fact is also reflected
in the amounts of energy transferred to various materials (see Table I I I ) .
I t may be concluded, at least for WR-1 geometry, that as
the number of regions is increased the dose ra te approaches a certain
value, and that 26 regions yield resul ts suff ic ient ly close to th i s
value.
4.3 THE EFFECT ON THE RESULTS OF TRANSPORT CORRECTIONS
The assumption that e l a s t i c scat ter ing is isotropic in the
laboratory coordinate system is adequate for scat ter ing of neutrons off
heavy nuclei (A >> 1). In such cases the laboratory and the centre-of-
mass coordinate systems are close to being iden t i ca l . But as the mass
of the struck nucleus decreases, the assumption becomes less sa t i s fac tory ,
and forward sca t te r ing by l ight nuclei cannot be ignored. In NEVEMOR,
forward sca t t e r ing due to hydrogen, deuterium, carbon, and oxygen is
considered by applying transport corrections.
To estimate the error involved in not considering forward
scat ter ing due to l ight nucle i , two computer runs using WR-1 geometry
data* were made; one with t ransport corrections applied, and the other
without any transport correct ions . For both cases the group-to-group
ine la s t i c cross sections for U-238 were used. From Table IV, i t i s seen
that the t o t a l energy transferred to a l l the materials in the ce l l is
not affected. (This is because albedo a = 1.) Since the neutron sources
( f i s s i l e material) are concentrated in the inner regions of the c e l l ,
* See Appendix 6 for geometry data.
- 36 -
TABLE IV
COMPARISON OF VARIOUS QUANTITIES FOR TWO CASES: FORWARD SCATTERING
APPLIED,, AND FORWARD SCATTERING NOT APPLIED
Forward Scat,Considered
Forward Sca t .Not Considered
Difference (%)
Total energy t ransfer red(watts)
20.388 20.238 -0.74
Outward energy flow throughcell boundary (watts)
8.842 8.041 -9.1
Energy transferred to hydrogen(watts/gram)
Region No.
-
= 1
6
13
24
26
Effective nickel-flux(1013n/cm2.sec)
Region No. ,1
13
26
2.555
2.601
2.136
0.553
0.454
2.694
2.738
2.252
0.531
0.417
+ 5.44
+5.27
+ 5.43
-3.98
-8.15
0.910
0.790
0.134
0.942
0.818
0.124
+3.52
+3.54
-7.46
- 37 -
S t o 1 3
u-vc
OCE
ID
n 1 r ] T
FORWARD SCATTERING APPLIED
G FORWARD SCATTERING NOT APPLIED
10I2L5 S 7
RADIUS (cm)
_L I L8 9 10 12
FIGURE 4: Comparison of Integrated Flux vs Radius for Two Cases:Forward Scattering Applied and Forward Scattering Not Applied
- 38 -
the effect of forward scattering is to enhance the neutron flux in the
outer regions while depressing it in the inner regions (See Figure 4).
This fact is also reflected in the value of the eiu-rgy flow out of the system
at the outer boundary of the cell. The effective nickel-flux and the energy
transferred to various materials, e.g., hydrogen, in different parts
of the cell indicate the same conclusion.
4.4 TIP; EFFECT ON THE RESULTS OF USING AVERAGE!) INELASTIC
SCATTERING CROSS SECTIONS
An incide.it neutron of a given energy excites various
nuclear levels of the target nucleus with different probabilities
through inelastic scattering collision. Subsequently, scattered
neutrons would have an entire spectrum of energy. Thus, for a
rigorous treatment of the slowing-down of neutrons, group-to-group
inelastic cross section matrices should he used (see Section 2.2),
Since these cross sections are cumbersome, such a matrix is used only
for U-238 in NEVEMOR, U-238 being the most important of all the reactor
materials as far as inelastic scattering of neutrons is concerned.
Computer runs were made using KR-1 geometry data* to estimate
errors involved in using averaged cross sections instead of the group-
to-group matrix for U-238. Output energy spectra for these two cases
are compared in Figures 5 and 6 for two sp;i ial regions. The two spectra
are similar except in the region of 0.5 to 1.5 MeV. Also, it can
be seen from Tables V and VI that all the energy values are the same
within less than one percent for the two cases.
Thus, the errors involved in using averaged cross sections
for U-238 in NEVEMOR are small. Since the inelastic scattering cross
section is much larger for U-238 than for any other reactor material,
* See Appendix 6 for geometry data
- 39 -
it cna be concluded that errors due to averaged cross sections for
all other materials are negligibly small.
TABLE V
COMPARISON OF
ENERGY TRANSFERRED TO VARIOUS MATERIALS IN THE CENTRAL DOSIMETRY HOLE
FOR TWO CASES: GROUP-TO-GROUP CROSS SECTIONS USED FOR U-238, AND
AVERAGED CROSS SECl IONS USED FOR U-238
Material
Hydrogen
Deuterium
Carbon
Oxygen
Aluminum
Iron
Zirconium
Uranium-235
Uranium-238
Inelastic ScatteringMatrix Used
2.555+
0.882
0.0395
0.0244
0.00826
0,00207
0.00126
0.000216
0.000226
Averaged CrossSections Used
2.569
0.884
0.0398
0.0242
0.00829
0.00?08
0.00127
0.000216
0.000227
Difference (%)
+ 0.5S
+ 0.23
+ 0.76
-0.82
+ 0.36
+ 0.48
+ 0.79
0
+ 0.44
t All energies given in watts/gram.
GROUP-TO-GROUP MATRIX (5IGIN) USEO
O AVERAGEO CROSS SECTIONS USED
I
o
1010
NEUTRON ENERGY (K'eV)
FIGURE 5: Comparison of Energy Flux Spectra for Two Cases: Group-to-Group Cross-Sections usedfor U-238, and Averaged Cross-Sections used for U-238 (for central dosimetry hole, I
10GROUP-TO-GROUP MATRIX (S 16 IN) USEO
O ÛVERÛGED CROSS SECTIONS USED
i—
10'PL. _
NEUTRON ENERGY (MeVI
FIGURH Comparison of Energy Flux S p e c t r a for Two C a s e s : Group- to-Group C r o s s - S e c t i o n s usedfo r U-258, and Averaged C r o s s - S e c t i o n s used fo r II-238 ( f o r fuel r e g i o n , I = 13)
- 42 -
TABLE VI
COMPARISON OF VARIOUS QUANTITIES FOR TWO CASES: GROUP-TO-GROUP CROSS
SECTIONS.USED FOR U-238, AND AVERAGED CROSS SECTIONS USED FOR U-238
Total energy transferred
Outwardthrough
energy flowcell boundary
Inelastic ScatteringMatrix Used
20.388+
8.842
Averaged CrossSections Used
20.404
8.839
Difference (%)
+0.08
-0.03
Energy los t through 0.756lower energy bound
Energy t ransfer red to mater ia lsin the en t i r e c e l l :
Hydrogen 2.132
Carbon 0.503
U-235 0.00109
U-238 0.0484
Energy Transferred to mater ials 16.942outside pressure tube
Effective Ni-flux(1013n/cm2 .sec):*
Region No. 1
6
24
Computer memory used
Computer time (sec)
0.910
0.933
0.165
106K
72.53
0.759
16.950
+0.40
2.143
0.505
0.00110
0.0485
+0.52
+0.40
+0.92
+0.21
+0.05
0.908
0.931
0.165
104K
65.12
0
0
0
-
_
t All energies given in watts.
- 43 -
5. APPLICATIONS
NEVEMÛR can be used to calculate the fast neutron flux
spectrum and energy transferred from fast neutrons to various materials
in any cylindrical system or approximation thereto. Besides minor
limitations due to various assumptions*, the validity of the calculated
values depends upon two important conditions. Firstly, the system
should be such that homogenization in annular regions does not take the
problem too far away from reality. Secondly, it should be possible
to specify the conditions at the outer boundary of the cell, viz., albedo
and/or incoming neutron currents at the boundary. If the cell geometry
repeats itself periodically to large distances, one can assume albedo
(a) equal to unity. Here large distance means more than three times
the slowing-down distance of the fast neutrons, (about 11 cm in heavy
water).
5.1 WHITES!ELI REACTOR NO. 1 (WR-1)
WR-1 core has a hexagonal lattice with a pitch of 23.5 cm.
Each fuel cell is cylindrical with an effective radius of 12.3359 cms, and its
details are shown in Figure 7u. For such a geometry, homogenization is a
satisfactory approximation, and if the cell under consideration is not at the
periphery of the core, albedo can be assumed to be unity with negligible error
in the results. The energy range from 10 MeV to 0.1 MeU is divided into 50
groups, while neutrons with energy more than 10 MeV belong to group 1.
Various differential neutron cross section data (see Appendix 6) are
derived from References 6 - 12. The fuel cell is divided into 26 annular
regions. See Figure 7b and Appendix 6 for geometry data. For this case,
the transport correction for light nuclei is applied, and the group-to-
group inelastic cross section matrix for 11-238 is used. The results
* See Section 2,1.
- 44 -
Nota ; All diminuons In cmRadii art mtoturti from bundltctntrt ocipt «h«ri otturmit indicated
FIGURE 7a: WR-i Fuel Cell Geometry (stainless steel pressure tube,large calandria tube)
- -45 -
FIGURE 7b: WR-1 Fuel Cell Geometry ( s t a i n l e s s s t e e l p ressure t u b e ,large c a l a n d r i a tube) showing Annular Regions used inNEVEMOR
- 46 -
are normalized to 1.0 kW power produced per 1 cm thickness of the cell
and are presented in the following graphs and tables.
The effective nickel-flux and the integrated flux vs average
radius are presented in Figure 8. Figure 9a shows the histograms of
neutron flux vs energy (group) for the central dosimetry hole, and the
moderator region. Figure 9b shows the same spectra except that here
the ordinate is flux per unit energy obtained by dividing the corresponding
values of Figure 9a by width (AE) of the associated energy group.
Except for those in Figure 9a, all energy spectra in this report are
of the latter type. The dip present in both the spectra at about 0.4 MeV
is due to resonance in the elastic scattering cross section of oxygen
and to a lesser extent of iron.
Table VII lists results of various energy calculations.
Here the 'Total energy input1 is the energy introduced by fast neutrons
from fission into the system. The 'Total final energy' is made up of
all the eventual distributions of the neutron energy, and its equality
to the input energy suggests that the calculations are at least self
consistent. The 'Total energy transferred' is the fast neutron energy
transferred to all the materials in the entire cell. As seen from
Table VII, the majority of the energy is transferred to materials outside
the pressure tube. NEVEMOR also calculates the neutron energy leaving
the cell through the outer boundary. Since albedo is assumed to be unity,
the incoming energy flux at the cell boundary is then equated to this
outgoing energy flux. The 'Energy lost through lower energy bound'
(0.756 watts), for WR-lt amounts to about 3% of the 'Total energy input'.
This energy, as mentioned earlier, should be distributed amongst various
materials according to their mass number and their macroscopic elastic
cross section, say, at 0.1 MeV. However, the 'Non-center-of-inass energy
in absorption reactions' (1.062 watts) is not transferred to materials
as kinetic energy but appears as radiation (e.g., gamma-ray) energy.
Table VIII gives energy absorbed by various materials in the central
dosimetry hole. Variation of energy absorbed by hydrogen (W/g) with
radius is also shown in Figure 8.
k—i
CO
era
n03l — i
83
Q .>-J
C"
f — f
- j -
ra. •
'?,—,
c'Jl
o
rrj«—•
'*/3
i - t
n
oo
=To
oc
X
. - *
r.7T
'—'
-r., .cX
5
o
!—_
OJ |—
i• * ^
33 " » > -
o
, ,r - i
3
QD i
E>
2mj
o_j >
œo33CD
moCD
I
ooom2
o
nm
i
"Tl|—cx
X
HnO
-ni
cX
~ C
O
o
O
NEUTRON FLUX (n/cm2 sec)
t>
t>
t>
oo
o
o
t>
oo
D>
ENERGY ABSORBED BY HYDROGEN (W/g)
CENTRAL HOLE (AIR)- ZIRCONIUMCOOLANT
FUEL+
C00LAN1
-^-COOLANT=—-PRESSURE TUBE (IROW
C O ,
--«-CALANORIA TUBE(ALUMINUM)
O IP10
a.
10'
MODERATOR REGION
(1= 24)
...A I..' J4 5 6NEUTRON ENERGY I M e V l
CENTRAL DOSIMETRV HOLE (1 = 1
i
i
10
FIGURE 9a: Fast Neutron Energy Histograms for WR-1 Fuel Site (stainless steel pressure tube,large calandria tube)
zoŒ
10"
CENTRAI D05IMETRY HOLE [! = I )
\
MOOERATOR REGION
il» 24)" \
I 1 i4 5 6
NEUTRON ENERSV I M i V )
l \10
FIGURE 9b: Fast Neutron tinergy Spectra for IVR-1 Fuel Site (stainless steel pressure tube,large calandria tube)
- 50 -
TABLE VII
VARIOUS ENERGY VALUES FOR WR-1 FUEL SITE
Total energy input 25.214t
Total f ina l energy 25.251§
Total energy transferxed 20.388*
Energy flowing out of c e l l 8.842
Energy flowing into ce l l 8.842 (since i=l)
Energy lost through 0.756*lower energy bound
Non-center-of-mass energy 1.062*in absorption react ions
Gamma-ray energy in 3.045*inelastic scattering
Energy transferred to 16.942materials outside pressure tube
Energy transferred to hydrogen 2.132in the entire cell
Energy transferred to carbon 0.503in the entire cell
t All energies given in watts
§ All asterisked quantities add to give 'Total final energy1
- SI -
TABLE VIII
ENERGY TRANSFERRED TO VARIOUS MATERIALS IN THE CENTRAL
DOSIMETRY HOLE OF WR-1 FUEL SITE
Material
Hydrogen
Deuterium
Carbon
Oxygen
Aluminum
Iron
Zirconium
Uranium-235
Uranium-238
watts/gram
2m
0.
0.
0.
0.
0.
0.
0.
0.
555
882
0395
0244
00826
00207
00126
00021b
000226
- 52 -
From energy absorbed by hydrogen and carbon, one can easily
calculate energy absorbed by cyclohe.xane (CfjHi2). For the central hole,
thi^ is calculated to be 401.7 mW/g (normalized to 1.0 kW/cm reactor
fission power). This value is in good agreement with 384.9 mW/g from
the measurements of M. Tomlinson et al. '3 The difference is less than
5%. Another quantity of interest is the energy absorbed by the organic
coolant*. N'EVEMOR yields a value of 3.184 W/cm per 1.0 kW/cm reactor
p ow e r.
It is also easy to calculate contributions of the adjacent
fuel elements to flux or to dose rates. We have assumed all along that
albedo is unity. This means that the outgoing neutron current is balanced
by the incoming current. Thu incoming neutron current is mads up of
two contributions. The first contribution is due to neutrons originating
in the adjacent fuel elements and entering the cell under consideration
(and not being reflected back). The second contribution is due to neutrons
leaving the cell and being reflected by D-,0 of the adjacent elements
to re-enter the parent cell. Thus, by varying the value of albedo and
the outer radius of the unit cell, the contributions due to neutrons
originating in all the neighbouring fuel elements can be estimated. In
the central dosimetry hole, this contribution to dose rate is only 4.4% in
the case of hydrogen and 4.2% in the case of zirconium. Also, the effective
Ni-flux at this location is increased bv 3o0% due to all the neighbours,
while the integrated flux (from 0.1 to 10 MeV) is increased by 5.5%.
5.2 NRU REACIOR
NEVEMOR lias run for the NRU reactor at Chalk River Nuclear
Laboratory for the case of the fast neutron facility in position G-20
to calculate close rate in cyclohexane. The calculated value is 43.25 mW/g,
while Boyd's luJ experimental value is 47.37 mlV/g (for effective Ni-flux =
1012n/cm2.sec). This is a fairly good agreement considering that the
uncertainty in the CosS activity (effective Ni-flux measurements ) is
* Coolant is assumed to be C H j . ^ with hydrogen content of 8,6 wt%and density = 0.81 g/cm3, (See Ref. 13).
- 53 -
estimated to be ± 5% ! . Also, the value used by Royd for the radiolytic
hydrogen yield from cyclohexane, G(ll2), is somewhat higher. A better
value of G(H2) seems to be 5.0 rather than 5.2 at doses of 5 x ]Q:: uV/n,
(see Figure 10, Reference 15).
5.3 NRX REACTOR
NEVEMOR was also run for the NRX reactor at Chalk River for
the case of an annular uranium rod in a lattice position to calculate
the energy absorbed by cyclohexane (C6H-l2) from the fast neutrons. The
computed value is 40.75 mW/g, which can be compared with Boyd's 15 value
of 46 mW/g (for effective Ni-Flux = 1012n/cm2.sec). Here, again, arguments
similar to the NRU case above can justify the discrepancy between the
calculated value and the experimental value.
- 54 -
6. REFERENCES
1. Driggers , F .E. , A Method of Calculating Neutron Absorptions andFlux Spectra at Epithermal Energiest AECL-1996, Atomic Energy ofCanada Limited, (1964)
2. Ha l sha l l , M.J., Modifications to the Computer Code Epithet,AECL-1996 (Supplement), Atomic Energy of Canada Limited, (1966)
3. Evans, R.D.j, The Atomic Nucleus, Appendix B, McGraw-Hill BookCompany, I n c . , New \ o r k . , (1955)
4. Moteff, J.t Neutron Flux and Spectrun Measurements with Radio-activanta , Nucleonics, 20, 12, p 56, (1962)
5. Askew, J .R . , Mesh Rcauirnnt-ntp for Neutron Transport Calculations,AF.HW-M 760, United Kingdom Atomic Energy Authori ty, (1967)
b. Yif tah , S. and Sieger , M., Unclear Cross Sections, IA-980, I s r ae lAtomic Energy Commission, (1964)
7. Schmidt, J . J . , Neutron Cross Section for Fast Reactor Materials,KFK 120 (EANDC-E-35 11), P a r t I I and P a r t I I I , G e s e l l s c h a r t f t l rKemforschung , Germany, (1962)
8, l l o w e r t o n , R . J . , , Sem-Enpiriaal Neutron Cross Sections, P a r t I I ,UCRL-5351, Lawrence Radiation Laboratory, Univ. of Ca l i fo rn i a ,(1958)
9O Sher, R., Signa Center - Neutron Civs s Section Evaluation Group,Neutron Cross Sections in Zirconiwn, BNL-666, Brookhaven NationalL a b . , N.Y. (1961)
10. S t . ehn , J . R . , G o l d b e r g , M.D. , Magurno , B.A. , W i e n e r - C h a s m a n , R,.,Neutron Cross Sections, Vol 1, S u p p l e m e n t 2 , 2nd E d . , BNL-325,Brookhaven N a t i o n a l L a b . , N.Y. (1964)
1 1 . Kon i jn , J . and Lauber , A . , Cross Section Measurements of the A'i5 8
(n,p) Co 5 8 and Si2'* (nta) % 2 6 Reactions in the Energy Range 2.2 to3.8 MeV, Nuclear Phys ics , £8 , 2, 191, (1963)
12. P a s s e l l , T.O., "The Use of Nickel-58 and Iron-54 as Integratorsof Fast-neutron Flux" Neutron Dosimetry, Proceedings of IAEASymposium at Harwell, Vol. 1, page 501, IAEA, (1963)
13. Tomlinson, M., et a l . , Radiation Energy Absorption in WE-1: Measurementsat Low Power, AECL-2763, Atomic Energy of Canada Limited, (1967)
- 55 -
14o B o y d , A . W . a n d C r o s s , C . , Neutron Flux and Uoainetrij Mean-.in ••(.•>:<.•in an NRU Fast Neutron Facility, U n p u b l i s h e d r e p o r t , CI 2 3 2 ,Atomic Energy of Canada Limited, (i9f>5)
15. Boyd, A.W., e t a l . , Methods of Dosinetry ami Flux Mr uturrr:, .. ' «•»..'Their Application in the NRX Reactor, AliCL-2203, Atomi.: linerjjy ofCanada Limited, (1965)
ACKNOWLEDGEMENT
It is a pleasure to acknowledge the deep interest of
M. Tomlinson in this work, who not only instigated this investigation
but also spent many hours in discussions with both the authors,
We also wish to thank W.G. Unruh for his help in general,
and in particular for making available the energy group cross sections,
- 57 -
APPHXIHX 1
AN a n LINK or- INPUT DATA AND AVAIIAHU. e n IONS
1 . I N P U T DATA
A . O P T I O N ( I ) ( 1 = 1 , 4 0 )12
B . HNHRGY DATA
R e q u i r e s O P T l O N ( l ) = : o r Î
( i ) T . ' T H ( I ) ( 1 = 1 , 2 0 )A4
l i i ) I : L ( 1 ) , V K ( l ' ) , KLM, K I N , IMA I , NMAl , V-.UKF 1 f)„ 5 F ! ' . 7 ! 3 ]7, 1 3 1 3 1 3
( i n ) H L ( K J ( K = 2 , k L M )
F 1 0 . S
( i v ) T h i s s e c t i o n i s r e p e a t e d NMAT t i n e s .
(SUBSTIMRI-MMI ,1.11.= 1 , U . M I ' R ' M ) , AMASS I MIM< • "
C.
A4
S 1 G A ( M P R (F 1 0 . S
S I G l i ' M P R iF 1 0 . . '
S I G I IMI'K!ï i o . r.
I.GAMAf.MPRF 10. "'
(v ) R e q u i r e d
SOURCllk;F 1 0 . S
vi ] Requi r ed
SIG1N( I )F 10. S
GFOMhTRY DATA
R e q u i r e s OPTION!1
( i ) TITG:1)A4
i i ) N,13
M)
Ml
M'
•; \ |
or.
un
i i
<J
- i
FS.
1
i f NSOR
1 f \ 1 N
( ) r 3
i : F' s . 4
! K = 1 , K 1 . M )
I K - 1 . K I . M ,
i K - 1 . K l . M i
! } . - } , > l . M '
' ' '
( K = = ! > N S . » K
' l r l l > ' "
1 M.iRV
1 1 4 . "
( 1 i 1 )
( i v )
JL(I?
=1,N
! 1 = 1 , N " )
ivi M K C i l , . n , lli-NSil,.J) (J=l ,.JL{ I') 1 (1 = 1,N")1 3 M l . il
ivi I Required uni y if OPTION(41 = 1.
M N •. M i - 1 , MY".\
n . A r r i V A ' i I O N F O I L I I A I A
R e q u i r e s O P T l O N i . i O i t u , a n d r e p e a t e d f o r t h e n u m b e r
o f d i f f e r e n t f o i l ::.at r r i a i - .
( i t I AI.P. 1) , 1 = 1 , ' J : , MP.i, CRUS- . , r lAII , A, AL
Al 111 I K ' T. 1 1 1 . " [;t.i. " l-"ii.™
( i i ) Requ i rev.1 on l> i f MP.I - d .
S K ; A l ; ' k i i K - l . K l . M l
OFl'IQXS
OI'T I ON ( 1
O P T I O N ( 2 )
OPTION (.3")
OPTI O N ( 4 )
O P T I O N ( 5 )
0: l.nd ot pros',ram
1: New i;eoi:it.'t r\ d a t a only
2: New energy d a t a on 1 >•
3: Al 1 new dat a
4: No geonu-'trv or energy d a t a , c a l c u l a t i o n sbypassed
U: T r a n s p o r t c o r r e c t i o n s not a p p l i e d
I : T r a n s p o r t c o r r e c t i o n s a p p l i e d
0: No d a t a output
1: Geometry da t a ou tpu t only
2: Lneryy d a t a output only
3 : Al1 d a t a output
0: Uniform f lux assumed
1: F lux shape fed in
0: No f l u x out [nit
1: No f l u x p e r u n i t l e t h a r g y or energyo u t p u t
- S 9 -
0PTI0N(6 t o 11)
OPTION(12)
OPTION ( H to IS)
OPTION(16)
OPTION(17)
OPTION(18 to 23)
OPTION(24 to 27)
OPTION(28)
2 : F l u \ p r r n i ; ! T ' - n e i v . • • • . . - i t p : ; t
3 : F l u x p e r n u i t l e t h a r v . y o u t p u t
4 : F l u x p e r u n i t let har , ;v ,iml u n i te n e r g y mit put
= I : R e g i o n - n u m b e r s fo r wh ich f l u x s p e c t r aa r e o u t p u t
= 0 ; I n t e g r a t e d f l ux v s . r a d i u s i s noto u t p u t
1: I n t e g r a t e d flu.x v s . r a d i u s '-- uni put
= MP : M a t e r i a l s t o w!n>\i f l u x : mwe i j;h t i'il and i s nut put
= 0 : K i n e t i c e n e r g y t r a n s i ' e r r e d not comparedt o e n e r g y l u s s e - ;
1: K i n e t i c enen. ;y t r a n s f e r r e d comparedt o e n e r g y ]o . ; s e s
= 0 : l ine r jjy b a l a n c e not done
1: I iner^y b a l a n c e done
= I : R e g i o n - n u m b e r s f o r w h i c h e n e r g y / ^ r a n .t r a n s f e r r e d and t o t a l e n e r g y t r a n s -f e r r e d f o r each m a t e r i a l a r : o u t p u t
= MP : M a t e r i a l s f o r winch t o t a l k i n e t i ce n e r g y t r a n s f e r r e d c a l c u l a t e d ando u t p u t
= I . \ „mm
Total iMierj'.y t r ans f e r r ed between
tliese l imi t s is ca ! m l at eilmax
= 0 : No fo i 1 t realed
= IO P T I O N ( 2 9 )
OPT I O N ( 3 D )
= Ni : N u m b e r o f r e g i o n s t h e f i r s tm a t e r i a 1 a p p e a r - - i n , ! \ ;
O P T 1 O N ( 3 1 t o ( .'SO+N i ) ) = I : R e g i o n - m i n i u - i - * ; i n w h i J i t l i ef o i 1 m a t i.'r i a 1 a p p e a r s
= 0 : No f u r t h e r f o i l s t r e a t e dOPTION(31+Nj'
= N . : N u m b e r o f re^ioir- ' h e -.i-i'oiul toilm a t e r i a 1 ajiptar-- i n , ( \ '"--'• >
O P T I O N f 3 2 + N , ) t o ( 3 1 + N j + N ; ) - I: I- ei; î o: -irimb. r- 1 1 • w : ;
OPTION(32+Nj+N;)
„„. etc.
OPT ION(40)
the1 s e c o n d f o i l m a t e r i a l a p p e a r s
= 0 , o r N , ('-' ',"-*•• y-
= 0: I - ' o i 1 n v . •• • '> t i i i - / - . i r - M i l . ' U !
I ; l u i 1 , r - •• • • • i l l •;; . m m i t ; . i t
- 60 -
APPENDIX
EXPLANATION OF NOTATIONS
1. NOTATIONS USF.D IN THE REPORT
Subscripts
J
k
Variables
A
c.
the subscripted quantity refers to region i.
the subscripted quantity refers to material j.
the subscripted quantity refers to group k.
atomic mass of a nucleus tin units of neutron mass),
the minimum fractional energy remaining with a
neutron after an elastic scattering reaction with
the j material.
the factor which normalizes the calculations to one
neutron in group 1 over the whole lattice cell,
number of collisions in zone (i,k) every second,
(sec"1).
lower energy bound of group k, (MeV).
average energy of neutrons in group k, (MeV).
an energy, (MeV);
Superscripts
p_rec£ding_ apostrophe ( !E): energy measured re la t ive
to the laboratory co-ordinate system,
absence_ of_th_is_ j>up_ers£rip£ (E) : energy measured
relative to the center-of-mass co-ordinate system,
£p2_l£win^ ap£stxrophe (E1): energy after a col l i s ion,
abs_enc£ of_this_ superscript (E) : energy before
the coll is ion,
bar_ oyer_E_(Ë) : average value of E,
y_ (E ) : energy associated with a gamma ray,
- (il -
Subscripts
j_(H.): kinetic energy associated witli a nucleus
of material j ,
n_(F. J : kinetic energy associated with a neutron,
c_(T:): energy associated with the motion of the
center-of-mass in the laboratory system.
H. , , , gamma-ray energy associated with an inelasticJ ,K , K
scattering of a group k neutron into group k' off
material j„
E. , ,, average kinetic energy transferred to a nucleus-1 • ' rh
of the j material due to group K neutron
inelastically scattering into group k' (as
measured in the laboratory co-ordinate system).
E. . , kinetic energy transferred to the j material in1 J J y K
region i from group k neutrons.F. . , gamma-ray energy associated with inelastic scattering
reactions of group k neutrons in region i with
material j which has group-to-group cross sections.
E energy lost to the system due to neutrons inelast-
ically scattering below the lower energy bound of
the system.
I:.' . eiiergv lost to the system due to group k neutrons1>J> ' til
elastically scattering off the j material inregion i below the lower energy bound of the system.
E', gross energy flux due to group k neutron currentK
at outer cell boundary;
x +: radially outward
x - : radially inward
F. input flux in group 1, region i.
4). average neutron flux m r.one (i.k), (cm 'sec ' ) .
tj,. average neutron flux in group k weighted to the
amount of material j in each region, (cm • sec ' ) .
I. . , number of group k' neutrons inelastically scatteringoff the i1"1 material into group k in region i per
orÏ , , second, (sec"1.).
- 62 -
,1. group k neutron current at the outer surface of1 j K
region i, (sec M .
+ superscript refers to the radially outward current,
- superscript refers to the radially inward current.
K number of energy groups considered.
K the last and the lowest group for which group-to-
group inelastic scattering cross sections are given,
first energy group consists of all neutron energies
above Ei. The number of absorptions in this group
would then be infinite unless some upper limit were
chosen. This upper limit for absorptions in group
one is ^E;, where „ is chosen to correspond to the
absorption cross section used.
N number of homogenised annular regions.
N. . atomic density of the j material in region i,2 u atoms/cm?).
N. . , number which is proportional to the number of1 » .1 > Kreactions or collisions per second o f a group k
th -1neutron with the j ' material in region i, (sec L).
x ~ I: inelastic scattering reaction which
leaves the neutron in group k.
x ; s: elastic scattering collision which leaves
the neutron in group k.
x = c: any reaction or collision.
q. • i,, i, number of group k' neutrons elastically scattering
off the j ' material into group k in region i per
second, (sec"1).
Q- , number of neutrons entering zone (i,k) due to
scattering collisions in higher groups in region
i, and due to sources in region i every second,
(sec"1).S. , number of source neutrons produced in zone (i,k)
* _
every second, (sec 1 ) .
S, number of source neutrons in group k produced every
second over the whole cell, (sec"1).
- 63 -
Ci. i t. microscopic cross section for a group k1 neutron
to inelastically scatter off material j into group
k, (barn) .x
o- k microscopic cross section tor a reaction x between
a group k neutron and material j , (barn).
x = E: elastic scattering
x H I : inelastic scattering
x - A: absorption of a neutron
x - t : any reaction
Y]- ,. macroscopic to ta l cross section in zone ( i . k ) ,
(cm"1).
8 neutron scat ter ing angle measured in the center-
of-mass co-ordinate system.
V. volume of region i , (cm3).X V
W.'[ the probability that a neutron which enters zone1 ,K
(i,k) by process x will undergo event y.
x = v: a scattering reaction in a higher group,
or a source, in region i.
x ; d: through the inner boundary of region i.
x = o: through the outer boundary of region i.
y ; v: a collision in zone (i,k).
y ; d: leaves through the inner boundary of
region i0
y = o: leaves through the outer boundary of
region i.2. VARIABLES USED IN THE PROGRAM
A* atomic mass of foil atoms.
ABSE neutron absorptions in group !„
This variable is also used as a dummy variable elsewhere in theprogram.
- 64 -
AL*
ALP
ALPHA [A)
AMASS(M)
AND RM
CMl\
COJ
CROSS
CS1(M)
D E N S ( I , J )
EBAR(K)
EEL
EEX
EGAMA(M.K)
EGAMT
EL(K)
ENIN
ETRAN(M.I)
ET RAT
F I N ( I )
I MAT
J J ( 2 , I )
J L ( I )
KIN
fractional isotopic abundance.
alphameric description of foil data.
maximum fraction of energy left to a neutron after
scattering e las t ica l ly from material Mo
atomic mass of material M.
normalization factor.
conversion factor from MeV to watt-sec.
neutron albedo of the material around the ce l l ,
mean neutron absorption cross section of foil
material.
average logarithmic decrement associated with
material M.
atomic density of the J material in region 1.
average energy of neutrons in group K.
energy flux through the lowest energy bound.
non-centre-of-mass energy in absorption reaction.
average gamma-ray energy due to ine las t ic scat tering
of group K neutron off material M.
tota l gamma-ray energy due to ine las t ic scat ter ing.
lower energy bound of group K.
source neutron energy entering the system.
neutron energy transferred as kinetic energy to
material M in region 1.
total kinetic energy transferred to a l l the materials
in the ce l l .
input group 1 neutron flux in region I.
material to which SIGIN is assigned.
neutron in-current at the I surface.
neutron out-current at the I surface.
number of materials in region I , (JL(I) .? 20).
If JL(I) > 100, then LIKE(I) = (JL(I)-IOO) is
the region which I duplicates.
lowest energy group for which group-to-group ine las t i c
scattering cross sections are assigned.
* This variable is also used as a dummy variable elsewhere in theprogram.
KLM number of energy g r o u p s ,
MPJ m a t e r i a l r e f e r e n c e number of f o i l m a t e r i a l ,
MRC[I,J) material identification number for the J material
in region I,
N number of regions.
NSOR number of energy groups i n t o which s o u r c e neu t rons
e n t e r .
OPTION(I) one of 40 o p t i o n s .
PHI( I ,K) a v e r a g e neu t ron flu.x in r.one ( I , K ) .
PIUH(K) f l u x pe r u n i t energy in zone ( I , K ) .
PHTK(I) i n t e g r a t e d f lux in r e g i o n 1,
PIIIL(K) f l u x p e r un i t l e t h a r g y in zone (_ 1,K).
PHIW(K] weigh ted average f lux with r e s p e c t t o a m a t e r i a l
component.
QF(I) number of neu t rons e n t e r i n g zone ( I ,K) due t o
s c a t t e r i n g c o l l i s i o n s In h i g h e r groups in region I ,
and due t o sou rce s in reg ion I .
R( I") o u t e r r a d i u s of r e g i o n !„
S ( I ) o u t e r s u r f a c e a rea of reg ion I .
SEL net energy f lux at t h e ou t e r boundary of the l a t t i c e
c e l l .
SELI g r o s s energv flux i n t o the c e l l at the o u t e r boundary
of t h e l a t t ice eel 1
SELO g r o s s energy f l u x out of the c e l l at the ou te r
boundary of t h e l a t t i c e c e l l .
SIGA(M,K) a b s o r p t i o n c r o s s s e c t i o n for m a t e r i a l M for neu t rons
in group K.
SIGAF(K) a b s o r p t i o n c ross s e c t i o n for f o i l m a t e r i a l for
n e u t r o n s in group K.
SIGAT(I) macroscopic a b s o r p t i o n and i n e l a s t i c s c a t t e r i n g
c r o s s s e c t i o n for n e u t r o n s in zone ( I , k ) ,
SIGE(M.K) e l a s t i c s c a t t e r i n g c r o s s s e c t i o n fo r m a t e r i a l M
f o r neu t rons in group K.
- 66 -
SIGET(l)
SIGI(M,K)
SI GIN IN'I
SIGSUM(K)
SIGTT(I,K)
ST(I.K)
SOURCE(K)
SPDL
SRAV
TAU
TCOL
TSCOL
TITE
TITG
WXY
macroscopic elastic scattering cross section for
neutrons in zone (I,K).
inelastic scattering cross section for material
M for neutron in group K. When the neutron undergoes
an inelastic scattering reactiont it loses any energy
EGAMA(M,K) to a gamma ray.
inelastic scattering cross section data in the
order o , J . c , . .2 > N x N 3 » 'J 3 » 'I
GKIN,KIN-^3,KIN' ak
KIN
E -macroscopic total cros.. section for neutrons in
zone (I,K).
number of source neutrons entering group K.
slowing down density at the lower bound o: group 1.
total number of source neutrons entering zone (I,K).
half-life of an activated foil atonu
proportional to total number of collisions in
zone (I,K1,
proportional to total number of collisions in zone
(IjK) causing secondary- neutrons.
alphameric description of energy data.
alphameric description of geometry data.
the probability that if a neutron undergoes a
process X it will undergo an event Y
X H 0: enter zone (I,K) from outer surface.
X = I: enter zone (I,K) from inner surface.
X î V: enter zone (I,K) due to a fission or
collision in region 1»
Y : 0: leave region I by outer surface.
Y = I: leave region I by inner surface.
Y = V: a collision in zone (I,K).
- 67 -
APPENDIX 3
NORMALIZATION FACTOR ANORM
If E. is the U-235 fission-energy per fission and v is
the average number of neutrons produced per fission, then EJv is the
fission energy per virgin fission-neutron. If S is the number of
virgin fission-neutrons per second per centimetre thickness of
lattice cell,) then SE_/v is the U-235 fission-power produced per
centimetre thickness of lattice cell. If one wishes to normalize
the results of the reactor calculations to x kilowatts of U-235 fission-
power per centiirietei thickness of lattice cell, one then multiplies
the results by the factor
ANORM = v-gv i i. , vrhere E~ is in kilojoules.
For NEVEMOR, S is calculated assuming a virgin fission-
neutron spectrum1-2 , F(E), defined by
F(E) = exp (-E/0.965) sinh /(2.29E) ,
which is normalized to one fission-neutron above 10 YieV per centimetre
thickness of the lattice cell»
- 68 -
APPENDIX 4
SIMPLIFIED FLOW CHART OF NEVEMOR
\ IF OPT'ONUI.Jotî
CALCULATIONS
OfRT«IN!Na TO
E4CM BEOION:
5 , v , 4 V B , » C E L
y<f J L ( 1 1
\
•h
\
> i o
/
' i E T u P R E 01
j \ TO SE
/ T O REÊI
/ JL III -
IOEN'
ON
1 0 0
L
0 ^/
X
0 H I
J
1tk
\ /\ IN?UT /
' \ OENS U, J ] /
\ MRC I I . J 1 /\ /
r' / I F O P T I O N I Î I M /
AET JP FICTITIOUS/ • . U T E O I A L S FOB /
/ T R A N S P O R T /
/coBnecTio«s /
I N I T I A U I I » U
P2RTINENT
BC'ORC 9TARTIN0
CALCULATIONS
0 0 •<
CALCUi ATE
Q U I N T I I I E ; RELS'ED
TT GROUP I
NEUTRONS S L O « .
1 0 DOWN DUE T 0
ELASTIC SCATTIRINQ
(SOOJIt, Jl I
CALLAVENS (N,rt ,«IN, "
WrttCHCUIATE3 NEUTRONS '
.OWING Ù 0 4 NNTO QROUP
CALCULATE
EN IN
ADO SOURCE NEJT
SONS TO OF ' p
'AtCULATE NEUTP.ONS
1LO«INI1 0 0 * N
INTO 3N0'jP I
CALCULATERENO i j9 ,
THE NORMALIZATION
TO ONE NEUTBON
ABOVE 10 "11
I CALL/LENOSI lN.COJ,
/HOPE, « I WK.CM\CALCULATt5 NEUTRON\ CURRENT^ AND
PROBABILITIES/VCâLÎULATE
AVERAGE NCUTRON
* LU'- , PMI ( I , P» I .
ANO J I L I , « t i O
NORMAL IJE
THE F L Ul
IN «IIOUP I
- 69 -
r~S57
Y
^OPTION (91 =0
ICALCuiATE THE 1iENERGY PER SECOND \
5 1 * TRANSFERRED TO ONII — ' SRAM OF E VE R V k
* MATERIAL FOB ATMOST 6 REGIONS
E.NIROY/5EC GMTRANSFERRED,
"" ETfWN I MP. 11FOR AI
M05T 6. REGIONS ;
. O P T I O N ( 1 2 ) • 0
AN (MP 1)
O J T P J T
\ THE ENEROY
^ JUST
CALCULATED
SUM OVER THCWHOLE CELL rHtENERGY TRANSFERWC
' TCI EACH OF AT MOST4 MATERIALS
! CALCULATE THE
INTEGRATES NCUTRO^
FLUX IN EACH |REGION I
\ FLUI
* fc 0
v S
l A i
EVRAN
1
E
O P 1
. C U L O '
( MPEEx
TflflT
r
ION lifi i
t
. 1 1
CALfULATE THEFLUX PER UNIT
V
--RTIOM 'EQUALS
0
! TOTAL FAST NEUTRONENERGY TRANSFERORTO MATERIAL* 'M THfAN^UluS DCFINET B'r H f S F O P T I O N * . I»;
T I 0 N I 5 ' • ? > * " LETHARGY FOR
AT MOST 6 REGIONS\ / PHIL ( K ) j
CALCULATE THEGROUP ! COTO ENIN. CEEL.SE_
CALCULAIT THE
FLUX PER UNIT
ENERGY FOR I T
MOST 8 REGIONS.PHIC ( K )
OUTPUT
PHIL 1«)
OUTPUT
CTRAT
SELO
\ SE L IS C L
\ e t L• 1
OPTlON(Sl i3
CALCULATE THl ,
i MATERIAL -WCIOHTEDl
! AVIRAOt FLUX, j
PWIWIK I .FOR ALL IMATERIAL? RC0UE3TH)
\ OUTPUT ,
\ PHIW ( K )
ERAP |K I
\ OPTlON(l7)rO > •
CALCULATEEGAMT,ENOUT
OUTPUT '
EN I N /
EN OUT il—
EOAMT iE e x
' THERE IS •
A TOIL TO BE
- TRE4TE0 .
INPUT
FOIL
•ATA
C A L C U I.ATEACTIVATION
IN EACH RCQICHSPECIFIED
OUT PUT
ACTIVATIONS
J
- 70 -
APPENDIX 5
LISTING OF NEVEMOR
cool
,002
Q003
0004
00050006000700060009001000110012
001300140015001600170018001900200021002200230024002500260027002800290030003100320033003400350036003700380039004000410042004300440045004600470048004900500051
COMMUN/ALL/OPT I UN(40 ) , V ( 30 » iQFI 30 I
COMMON/LFN/Rt 30 I , S ( 3 0 ) , T ( 30 ) f J J t 2 , 30 1 t WVV ( 30 ) , WOVI 30 1 ,WI VCÎ0I ,1S1GTTI 30,60)CCMMON/KAV/VM 60) .UV160) , LIKE( 30» . JLI30I ,MRCO0,20) ,TFNS< 30,?0l ,
1 S I G 1 N ( 1 8 0 0 ) , S I G Ê ( 2 C , 6 0 ) , E B A R < 6 0 ) , EGAMA<20,60 I,SDUJ(30,20 ! ,2PHI(30.c.0l,4LPMA!2C)tAMASS<2C)fSlGI(20i60).CSI(20)DIME Ni I UN tL(60),SÎGA<20,60l,SIGSUM(60),AVR(30),F IN<30)iSOURCE(60)
l,TITEI2OI,r!TG(20l,SIGAT(30>,SIGET<3O),PHlKMO),PHIt(6Ol,PHIrf(ft0),2tTPANl 20,30 ) .SFGAFI 601 , A LP ( 9 ) , SUBST ( 2C , 4 ), 5UB ( 4 ) , MPR < ?0 I , PH I L ( b"> IRfcAL*4 JJINTEGFR*2 OPTIONE X T E K M i L HL1PL
C M W = 1 . 6 0 2 1 * 1 1 0 . ) * * l - 1 3 )100 READ ( 1,11)(OPTION!I I ,1=1,401
IF(OPTTON(ll-i)101,102,133101 CALL EXIT103 IFIOPTIQNl11.E0.4I GO TO 557COMMENT, INPUT THfc ENERGY DATA
READ ( 1,18) (T1TEI I ) , 1=1,20)RtAD(l.l2IEHlltVK(l»,KLM,KIN,IMAT,NMAT,NS0PREAD (1 ,13)IbLIK),K = 2,KLM)DC 120 K=2,KLMVMK)=EL( H-l I/ELIK)UV(K!^ALOG(VK(KI)
120 EBAR(K ) = ( E U K.-1 )-f L (K) I /LJVtK.1UV( l)=ALDGl V M 1 ) )DU IZZ M=l,20AMASS(H)=1.E+1OALPHA!M)=1.CS I (M)='J.DO 145 1=1,4
145 SUBSTIM,I 1=0.DO 122 K=1,KLMSIGA(M,K)=O.SIGE(M,K)=-O.SIGI(M,K)=O.
122 EGAMA1M,K)=O.DO 121 M=1,NMATREAD 11,33) (SUBII) ,1=1,4),MPRIM1,AMDO 128 1=1,4
128 SUBST«MPR(M),1)=SUBÎI)READ (1,131 (SIGA(MPRIM),K),K=1,KLM)READ (1,131 (SIGEIMPR(M) ,KI,K*l,KLM »READ (1,13) (SIGI(MPR(M) ,K),K=1,KLMJREAD (1,13) (EGAMAIMPR(M),KI,K>1,KLM)AMASSIMPR(M))=AMALPHA(MPRIM))=(AM-1.»*(AM-1.)/((AM+1.)*(AM+1.|)AL = ALPHA(MPR(,M) )IF(AL.EQ.O.) GO TO 127IFJAL.NE.l ) CS. I (KPRIM) I = 1. +ALOG( AL )*AL / «1.- AL )GO TO 121
127 CSKMPP.IHI ) = 1.121 CONTINUE
IF(NSOR.EQ.O) GO TO 148DO 137 K=1,KLM
137 SOURCE(K)=0.«EAD (1,13) (SOURCE(K),K=1,NSOR)
00520G53
0055005600570056005900600061
0063006400650C66006?00600069007000710072007300740Ù750076007700780C790080008100620083008V0065008600870C88008900900091009200930094009500960097009800990100010101020103010401050106010701C8
1 irt
129
126
[F ( S(U)M-L ( 1 I . fcO.O. ) GC TO 149oc i iM K ». = i, r.suP
SouRLf. (K ) = bUUP-LHK > /SPUPCE ( 1 Ilit TI • 1 <• h
WP1TE ! 3 ,4II H LJP t I L . M 2 I • t b > 0 ) GO TO 123OC 12 1 K - ! ,KLMOC U'? M= l ? , ? jSU.f ( H , - I = J (,,fc ( f - Q . K II l ! « n . ; u . n i GU DC 126M * n 1 N- — ! s - t l / iK l / > . ' i , 1 i ' i i , i b l N ! I ) , 1 = 1 , t c l IOG ! <J "•• K- = ;> , K l rj
l'L 1 , . . f . ' , > M , VI ••
ïf ( (i ^e b A -11•*(• i r t (W f- 1 T t
WP i T t
W P I T t (
h f i I T t (
KHTM00 i 4 <•w f -1 T e t
WkîT l1« M T [ (WO J T L (W R I T t (WPITF (*k]TE IWR 1 ï tI F ( M P «
i MAT .
r ;. * N <I = q ) M
3 , 1 I
l J , 2 (
3 , i<+ )
3 . 3 5 )3 , 3 1
3 , 363 , 3 73 , 383 , 3 73 , 3 ^3 . 3 73 , 4 0( 3 , i f( M I . M
,K)-SIGSUM(KI)»AMASS( I«AT I/1AMASSI ÏMATI + 1. )
1 l.tO.C J.DP. « 3PT!ONI3),EO. J.) I GO TO 105
) 1 T ] T H 1 ) , 1 « 1 , 2 0 )
NMA7< SUBST(MPR'.H) , 1 ) , 1 = 1 , 4 )(K.SIGAIMPPIMI ,K|,K=l,Kt«l
<SUBST1MPR(M),I),I=1,4)(K.S1GE(HPK(M) ,K) ,K=1,KLM|
(SUBST(HPRtM),I1,1=1,4)(K., S1GI I M P R { H ) , K Î , K = 1 , K L M )
1 S U b S T ( M P R i M ) , 1 ) , 1 = 1 , 4 1) ( K , E G A * A I M P R ( H ) , K ) , K » 1 , K L M )fc. IMAT1G0 TO 1 4 4
KR I T! ! 3 ,H? I K.KK-KlK'i K-Z!-(K-3)*K/2KF=KX»KIN-KDD 144 fJM=KX,K> , 10K 1 = K < N *< - K. XK2=NH
105
U-( (NM + 1 0 1 . G T . K F ) K2MAX=KF
WRITE- ( 3 , 4 5 ) ( I » [ - K 1 . K 1 H A X IrtPl T M 3 . ?3 I ( S I G I N ( l ) , i = K 2 , ! < . 2 M A X )CONTÎNUFIf- ( N S O P . E U . O ) l i d TO 1 0 5W R I T t ( 3 , 7 1Wf- ITF ( 3 , 2 2 ) IK. , SOURCE (K ) , K = 1 , N S O R II F ( O P T I U N C 1 ) . E 0 . 2 ) GO TO 1 0 6
COMMENT. I N P U T THE GEOMETRY DATA
-72-
01090110OUI01120113QU4011501160117011801190120012101220123012*01250126012?01280129QUOOUI01320133013*0135013601370138013901*001*101*201*3014*014501*601*701*801*90150015101520153015*015501560157015801590160016101620163016*0165
102
139
131
132
133
130
IS*135136
1*6
HEAD (1,181 (TITG(I»,I = 1,20)READ (1,151 N,C0J,EN0RMANOPM=ENORM*8.*23E*1OIF(COJ.LT..001I COJ=l.READ (l,10( (JL(IIt1=1,NIRCAD Jl.lt.) (R(l),l = l,N)V(1) = 3.1*159*{RU)»R<1M
S(1)=6.28318*RU»VCEL=3.1*159*R(N)*RIN>DC 130 1=1,NIF I I.EQ.L » GO TC 13<5V(II = 3.14159*(R( 1 I * R ( I » R ( I 1 I * R ( I 1 MAVRII 1=2.09439*1 M l ) *fi ( I ) *R( II -R « 1-1 )*RI1-1 I *R( 1-1 M /V « I IS(I>=6.28318*R(I IIFIJLi I I.GT.IOO) GO TO 133MAX=JL(I)READ (1.17) (MRC ( I , J I ,DbNS( 1 , J > ,.l»l ,WAXIIF(OPTILJN(2I.EQ.O) GO TO 132NU«=0DO 131 J=1,MAXIF t IMRCII ,JI.LT.8).0R.(MftC(I,Jl.GT.in I GO TO 131NUH=NUM*1J1=JL(i)+NUMMP=MRC1I,JIMRC1I,J1)=MP*1O9DENS(I,JIl=DENS(I,JI*(-2./(3.*AMASS(MP|lICONTINUEJL1I)=JL(II*NUMLIKEUI--0GO TO 130MP=JL(I)-IOOJLUMJUMP)LIKE(I)=HP
TO 13*l,Nt
1*1
DO 130 J=1,MAXMRC(I,JI=MRC(MP,J)DENSIÏ,J)=DENS(MP,J)CONTINUEIF(OPTION(*).EQ.O)GOREAD ( 1, 16)(F IMj I ) ,GO TO 13600 135 1*1,NFIN(I 1 = 1.IF((0PTI0N(3).EQ.0l.0R.<0PTI0N(3I.EQ.2»l GO TO 106WRITE(3,1)WRITE(3,*3)DO 1*6 M=1,NMATMRITE(3t** l (SUBST»MPR(M|,I I,I«1,*»,MPR(Ml,AMASSIMPR(M I )
1ALPHA(MPR(H!I,CSI(MPR(H)IWRITE (3 ,1 )WRITE(3 , *6 ) (T ITG( I I , I =1 ,2O IWRITE (3,5100 1*0 1 = 1 , NI F I L I K E m . E Q . O ) GO TC 1*1MRITE(3,6) I , F I N ( I ) , R ( I » , L I K E ( I IGO TO 1*0WRITE(3,2OI I , F IN( I ) , R( I I ,MRC < I » 11 t O E N S d t l l
01660167C1-S30169017001710172017301740175
01760177017801790180018101820163018*018501860167
0188016901900191019201930194019501960197019B0W90200020102020203020402050206020702080209021002110212021302140215021602170218021902200221
I.Ea.1IG0 TO 140MAX»JL(I IIFIOPTIONC2I.EQ.0I GO TO 142DO 143 J«2»MAXI f M M R C U , J I . G T . 1 1 6 J . A N D . (MRCI I , J ) . L T . 1 2 1 > ) GO TO 143WRITE < 3 t 2 l ) J , M R C ( I . J ) , 0 E N S I ! , J )
143 CONTINUEGO TO 1 4 0
142 WRITE (3,211 iJ,MRC(I,Jl,DENS(I,J),J=2,M4XI140 CONTINUECOMMENT. INITIALIZE SOME VARIABLES1G6 ABSE=Q.
SPOl«O.EMN-0.ETRAT»O.£EX=O.fcfL=0.SLL*O.SElI*O.SELO=O.EGAMT»O.Tf=O.S R A V S ' l .
COMMENT. CALCULATE THE SECONDARY NEUTRONS AND MACROSCOPIC CROSSDO 160 K - l . K L MDO 150 1 * 1 , NSIGAT1 I 1 = 0 .S 1 G E T I 1 1 * 0 .S I G T T J I , K I » O .TCOL=O.TSCQL=O.M A X * J l J I >DO 151 J«1,MAXMP=MRCtI tJ»If-i i (HRCJ I r J i . L T , 3 0 0 ) . Q P . Î K . E Q . I I I . O P . < K. GT.K IN) ) GO TO 153MP*HP-300
153
TCOL=TCOL*DENS<I (J)*ISIGAfMP ,KI*SIGE<MPiKi»SiGIIMP tKM*UV(K )IFMMftCI I, J».LT.100».0R. (MRCII , J ) .GT. 200 » ) G O T O 154TSCOL=TSCOt*DENS(ItJ)*S1GEIMP,Kl*UV!K)GO TO 155
15*. IF(VMK)*AL.LT.l.) GO TO 156TSCOL-TSCOL + DENSU.JI^SIGECMP.KI^UVItO-AL^ALOGIAD/ALl-l. IGO TO 1 5 5
156 TSCOL=TSCOL*OENS(I,J»*SIGEIHP,K)*(UVIK)»1./VK(K>-1.I/AL1155 SI GAT( II = SIGAT( I}*DENS(I.JI»(SIGAiMP,K)»S1GHMP.K) )
SI GET I i» = SIGET(1J*DENS(I,J)»(SIGE(MP ,K) I151 CONTINUÉ
IFISI&ATIII.LT.I.0000001 11 S I GATtIt=.0000001SI&TTtI,K)=SIGAT(I»*51GET t I I
TCOL*DENS(I «JI»UV«K>*SIGSU"(K)TSCOL = TSCOL*DENS(1»J)*UVIK)»SI GIN( KX )SIGATI1) = SIGiT(II+DEN II,J )*SIGSUM(K)IF1MP.GT.200) GO TO l.-lIMMP.UT.10QIMP=MP~100
-74-
022202230224022502260?.270228
02290230023102320233023*»023502360237023802390240024102420243
024402450246024702480249025002510252025302540255
0256025702580259026002610262026302640265
0266026702680269027002710272
02730274
IF(SIGTT< I ,K).LT.U0OOOOl> » SIGTTII ,K I =. 000001IFUC0L.E0.0.1 GO TO 157T( I ) = TSCOL/TCOLGO TO 1 5 0
1 5 7 T ( I » = O .1 5 0 CONTINUE
I F I K . G T . 1 1 GO TO 161COMMENT. 00 THE GROUP ONE CALCULATIONS
00 170 1=1 ,NTF=TF*FIN( I » * V U )Q F U ) = 0 .MAX=JL(I)DO 171 J=1,MAXMP=MRC<I,J»!F (MP.GT,300» MP=MP-300IF (MP.GT . IOO) GO TO 171SOOJ( I , J > = C S I ( M P » * D E N S I I , J ) * S I G E I M P , 1 ) * F 1 N < J ) * V I I iSPDL=SPOL+SOOJ( I , J>AL=ALPHA(MP»I F U V K ( 2 > * A L ) . L T . 1 . ) GO TO 172QF<I) = QF( I ) *S0OJ( I t J )GO TO 1 7 1
1 7 2 0 F i n = O H I > + < ( < V K ( 2 ) - 1 - W V K 1 2 J ~ A L « U V « 2 » » / « 1 . - A L » I * S I G E < H P ,l D E N S H t J ) * F I N ( I ) * V ( I t
171 CONTINUE170 ABSE=ABSE*UV(1)*FIN(I1*VII>*SIGAT(!»
RENO=l./(SPDL*ABSe)ABSE=ABSE*RENOSPDL=SPDL*RENODO 173 1*1, N0F(I»=QF(I)*RENOMAX=JLtItDO 173 J=1,MAXSD0J1I,J»=SOOJ(I,J)*RENi
173 CONTINUEGO TO 160
COMMENT. CALCULATE THE FLUX I N ALL THE OTHER GROUPS161 I F I K . G T . 2 » CALL R A V E N S ( N , K ( K I N , E H K » )
00 163 1 = 1 ,NSRAV=SOURCE» K » * F I N ( I ) * V ( I » / T FSRAVS=SRAVS*SRAVQ F ( I ) = Q F ( I ) * S R A V
163 ENIN=ENIN+SRAV*EBAR(K)' CALL LENORE(N,COJ,HOPE,K)
PHI(l,KI=(QF<l)*WVV(l»*JJ(l,l)*WOV«ilI/(SIGTT(1,K |*V(1 I IDO 164 1=2,N
164 PHKI ,K) = (QF( I »«WVV(I I*JJ( 1,I)«WOV( I )+JJ(2, 1-1 ) *WI V ( I ) I / (1SIGTTI I,KI*V«I) »SEL0=SEL0+JJ(2,NI*EBAR(K)SELI=SELI*JJ(1,N)*EBAR<K)
160 CONTINUEDO 165 1=1,N
165 PHI(I,1|=FINU)*J»ENO5 5 7 I F < 0 P T I C t N < 5 ( . E Q . O t G O T O 5 1 0
I F (OPT ION(121 .EQ.O) GO TO 500COMMENT. CALCULATE AND OUTPUT INTEGRATED FLUX
DO 508 I = l , N508 P H I K 1 I ) = O .
) *
027502760277027802790280026102820263028*0285
0286028702B802890290029102920293029*0295029602970298
02990300030103020303030*03050306030703080309031003110312031 1031*031503160317031803190320032103220323032*
032503?60327O32R0329
WRITE ( 3 , 1 1WRITE<3,50) ENORHWRITE ( 3 , 8 1DO 502 1=1,NDO 501 K=2,KLM
501 P H I M I ) = P H 1 M I » * P H I ( I , K >P H I M I > = P H I M I )*ANORM
502 M R I T E ( 3 , 2 * ) P H I K ( I I . A V R d )500 I F ( O P T 1 O N < 5 ) - 2 I 5 0 4 , 5 5 1 , 5 5 *55* DO 553 LM=1,6
I F < O P T I O N ( L M « - 5 » . E Q . O ) GO TO 551COMMENT. OUTPUT FLUX SPECTRA
WRITEO.l)WR1TE(3 , *7 )OPTION(LM*5»00 553 K=2,KLMPHtL(KI=PHlIOPTION(LM»5I,K|/UV(K»«ANOR«
553 WRITE(3,2*)PHIL(K) .EBARU»IF(OPTION(5I.EQ.3I GO TO 504
551 DO 503 LM=1,6IF(0PTIdN<LH*5I.EQ.O» GO TO 504WRITE(3,IIWRITE!3,9(OPTION(LM*5)DO 503 K=2,KLMPHIEIK)=PHIf 0PTION<LM+5>iK)/(EL<K)*(VK(M-l.H*AN0RM
503 WRITE(3,2*)PHIE(K»,E8AR(K)COMMENT. CALCULATE AND OUTPUT WEIGHTED FLUX50* DO 507 NN=1,3
IF(OPTI0N(NN*12».EQ.0> GO TO 510DENO=0.DO 509 K=1,KLM
509 PHIW(KI"0.WRITE(3.II00 50b I-l.NMAX = JL(I I00 505 J=l,MAXMP=MRClI,JIIF(MP.GT.300 IHP=MP-300IF«MP.GT*2OO)MP=MP-2OOIF <MP.GT.100)MP=MP-100IF(0PTIDN(NN*12).NE.MPI GO TO 505MX = MPDfcNO=DENO*DENS(I,J)*V(I>DO 556 K=2,K.LM
556 PHlfe(K)-PHIW(K)*PHI(IfK)*V(I)*DENS(I,JIGO TO 506
505 CONTINUE506 CONTINUE
Wfi I T E ( 3 , * B I ( SUBST(MX,L) , L = 1 , * IDO 507 K=2,KLMPHIW(K) = PHIW( K)*AN0R>1/<DEr4a*EL(K,l
507 WRITE13 .2 * ) PH IW(M,EBAR(K)510 IF (OPTia 'Jd I . E Q . * I GO TO 5 1 *COMMENT. PERFORM THE ENERGY CALCULATIONS
DO 550 M = l , 2 0DO 550 K=1,N
550 ETRANt M,K.(=O.WR ITEJ 3,1»WPITE(1 ,5O) ENORM
-. o-
03300331033203330334033503360337033803390340034103420343034403450346034 703480349035003510352035303540355
035603570356035903600361036203630364036503660367036603690370037103720373
0374037503760377
03760379
0380038103820383
516515513
552
555
512511
DO 511 1 = 1 t NMAX=JL(1)DO 512 J=lfMAXHP=MRC(I iJ)I H M P . I T . 3 O O ) GO TO 513MP=MP-300A=AMASS(MP)AL'ALPHAIMP»A L l = < A - l . ) / ( A * ( A » l . I >DO 515 K=2,K.INK X = K I N * ( K - 2 ) - K * ( K - 3 ) / 2FACTOR=O.KF=»KX*M N-KDO 516 KS»KX,K,FFACTOR»FACTOR*EBAR(KS-KX*K)/A*SIGIN(KS)ETRAN(MP,1) =ETRAN(MP,I)*PHKI,K)•(FACTOR*EBAR«K)*AL1»SIGSUMIKI >IF1MP.GT.200)MP=HP-200IF<MP.GT.100IMP«MP-100!F(OPTION(2 ».EQ.OI GO TO 552IF1MP.GE.17) GO TO 511A-AMASSIMP)AN«l,m.»A)ALl»l.-ALPhA(MPI00 555 K=2,KLMEEX«EEX*PHI(I,KI*EQAR(K)«StGA(MP,K»*AN*A*V(I)*DENS(1,J)ETRAN(MP,I )=ETRAN<MP,I)*PHI(ItKI*EBAR<K»*(SIGEIMP,K»*AL1*. 5*1SIG4(MP,KI*AN+SIGI(HP,K)*AL1*(.5-EGAMA(MP,K)*AN/(FBAR(K)*AL1)))ETRANIHP.t)=V(J)»DENS«I,J(*ETRAN(MP,I IETRAT*ETRAT»ETRAN(HP,I)CONTINUEIF(0PTION(161.EQ.0) GO TO 514Ei=Elil)EKL-ELIKLMI00 517 1=1fNMÛX=JL(I)DO 518 J«l,MAX
IF<MP 3GT.30O) MP=MP-300IF(MP.GT.2OO) GO TO 518I F I K P . G T . I O O ) GO TO 519
5 2 1
520519
AL = ALPHA(MP »AL1=1.-AL.ENIN=ENIN*.5»DENS(I,Ji*PHI(I,l)»V(I)*SIGE<MPf1(*AL1*E1IF(<E1*AU.LT.EKU EEL-EEL* . 5*DENSI 11J »*PHI (I ,1>*V( M*SIGE( MP , 1 )*
1EKL*(EKL/É1*-AL*AL*E1/EKL-2,*AL»/AL1DO 520 K=2,KLMIF((EL(KJ«AL).GE.EKL) GC TO 520IF((El(K-l)*AL).LT.EKU GO TO 521EEL-EEL-,5*0ENS(ItJI«PH1(I,K»*VtI»*SIGE<MP.K)/IUV(K»*AL1t*EKL*iEKL1/EL(K)*AL*AL*EL«K»/EKL-2.*AL)GO TO 520EEL-EEL*.5*0ENSUiJI»PHIU fKt*V(II*SIGE«MP,K»/<UV«R»*AL1l*«EKL*EKL
1*(1 . /EL(K) -1 . /EL(K-1H-AL*AL*«EL1K-1 I -EL(K) »)CONTINUEIF(MP.GT.IOO)MP»MP-1OOIF(OPTION(2J.EQ.O) GO TO 529I F ( M P . G E . i 7 ) GO TO 5 1 7
038403850386038703880369039003910392039303940395039603970398039904000401040204030404C40504060407040304090410041104X204130414
04150416041704180419042004210422042304240425042604270428
04290430043104320433043404350<*36043704380439
529 A=AMASS(MP>
518517
AN=A/<(A+L. ) * (A*1 . )>00 518 K=2,KLMFRAC=AM*EBARU)-AN*EGAMAJMP,K)lF<FRAC.LT.EKMEEL=EEL + DENS<I tJ I*PHI( I tK)*VU)*SIGMMP,K)*FRACCONTINUECONTINUEETRAT=ETRAT*ANORM*CMWEEL=EEL*ANORM*CMWSELO=5EI.0*AN0RH«CMWSEU=SEU*ANORM*CMWSEL=SELO-SELIWRITE(3,25» ETRAT,SELO,SELI,SEL,EELIF(OPTION(17>.EQ.O) GO TO 514DO 522 I = l f NMAX=JL< I IDO 523 J=1,MAXHP=MRC(I,JlIF<MP.LT.30O) GO TO 526MP=MP-300A=AMASS1MP)A M = l A * A + 1 . ) / ( A * ( A + l . I t
DO 525 K=2,KINKX=KIN*(K-2) -K»(K-3>/2
FACTOR=O.DO 524 KS=KX,KF
524 FACTOR=FACTOP*EBAR(KS-KX*K)*SIGIN<KSI52 5 EGAMT = EGAHT*DENS«I«J»*PHI< I ,K»*V»I)*(AM*EBAR(KI*SIGSUM(KI-AN*
1FACT0R)526 IF(MP.GT,200) GO TO 523
IF(MP.GT.IOO) MP=MP-1OOIF(OPTI0N(2),E0.0) GO TO 528IF(MP.GE.17I GO TO 522
528 DO 527 K=2tKLM52 7 EGAMT=EGAMT+DENSU,J)*PHI( I , KI«V U )*S IGI ( MP,KI*EGAMA ( MP,K )523 CONTINUE522 CONTINUE
ENIN=ENIN*ANORM*CMWEEX=EEX*ANORM*CMWEGAMT=EGAMT*ANORM*CMWENOUT=EGAMT+EEL*SEL*ETRAT*EEXHRITE(3,26I ENINfENOUT,EGAMT,EEX
514 WRITF(3,1)COMMENT. OUTPUT WATTS/GRAM AND WATTS TRANSFERRED TO MATERIALS IN CERTAIN REGIONS
DO 537 I N = l i 6I = 0 P T I 0 N ( 1 7 + I N )I F ( I . E Q . O ) GO TO 5 3 1MAX=JL(I)WR1 TE I 3 ,49 i IDO 530 J=1,MAXMP=MRC( I i J )IF( MP.GT.3O0)HP=MP-3OOIF(MP.GT.Z00)HP=MP-2 00IF(MP.GT.100)MP=*P-100IF(0PTI0NI2 l .EQ.OI GO TO 536
--'8-
04400441
0443
044504460447044a0449Û45Q04510452045304540455
04560457045804590460046104620463046404650466
04670468046904700471C4720473047404750476047704780479046004810462048304840485048604670468046904900491049204930494
IF(MP.GE.l7) GO TO 537536 ET=ETRAN(MP,I)*.6023/(DENSU,J»•V(I»*AHASS(MP>(•ANOR**CMW
ET1=ETPAN(MP,I)*AN0PM*CMW530 WRITEI3.27) ( S'ja ST ( MP , L ) ,L = 1,4 » , ET , ET l537 CCNTINUECOMMENT. OUTPUT TOTAL ENERGY TRANSFERRED TO CERTAIN MATERIALS531 DO 532 MAT=1,4
IF(OPTION(MAT*23».EO.OI GO TO 533ET*O,MP=OPTION(MAT+23JDO 534 I= L , N
534 ET=ET+FTRAN<MP, I )
5 32 WRITFI3,2B)fcr»(SUBST(MP,L),L=1,4»533 IFI(OPTrJN(28).E0.0).0R.(OPTIONS29».E0.0)) GO TO 540
I 1=OPTIOM(28)
CJMMENT. OUTCUT ENERGY TRANSFERRED BETWEEN REGIONS II AND IFFET = O.DO 535 ! = 1 I , IFF
535
DO 535 J=MP=MRC<I,JIIF(MP.GT.300) MP=MP-300IF(MP.GT.2OO) HP=MP~200IF(MP.GT.IOO) MP=MP-100fT = ET*eTRAN(MP , I I
WRITE! 3,2e?) I I , IFF,ETCOMMENT. CALCULATE: AND OUPTUT540
11=1,5
((3O*NO».EQ.4O)) GO TO 100
NICKEL ACTIVATIONS.N0=000 541NI=DPT I'JNI -)0IF((NI.EJ.O)HP I TF ( "i , 1 IWRITfc(3,50) ENORMRt AD( 1 ri1)) t ALP ( J) . J= 1,91 . M P J U C K O S S . T A U . A . A LHRI TF( 3,<.M ( ALP( Jl , J=l,9)IFJMPJ.F-J.O! GO TO 542DO 545 K-l , KLM
545 SIGAF(K)-jSGA(MPJ,KIGO TO 5^3
542 READ(1,13!(SIGAF(K),K=1,KLH)5 4 3 - IF(OPTION(<*O) .NE.O) W P I T E O . 3 0 1 ( K , S I GAF ( K I , K=l , KLM)
DO 544 L 1 = 1 , N II=OPTION(30+NO+LI)A B S F = S I G A F ( 1 ) * P H I ( I , 1 | * U V ( 1 )DO 546 K = 2 , K L *
546 ABSF=ABSF*S IGAF(K) *PHI ( I ,K )ABSF=ABSF*ANORMABSFT=ABSF*AL/(A«TAU)»,0250468PHIEF=ABSF/CROSSW R I T E ( 3 , 3 1 I A B S F T , I
5 4 4 W R I T E ( 3 , 3 2 ) P H I E F5 4 1 NO-NO*1*NI1 FORMAT(8H1NEVEHQR)2 FORMAT(28H-ENF.RGY DEPENDENT INPUT DATA//13 F0RMATU2H0CRGSS SECTION DATA AS A FUNCTION OF GROUP I
04950496
049704980499
0500
0501050205030504050505060507050805090510051105120513051405150516
45
67
e9
10111213141516171819202122232425
0517
0:521
0522
26
051605190520
272829
30
31
052i05240525
00260527052S0529
0530
0531
05320533
323334
35363738
39
40
4142
FORMAT) 15H-SOURCEUJ IS 0»FORMAT<30H-GE0METRY DEPENDENT INPUT DATA////3X,•1•,6X,•FIN(I I' ,6X,l'R (I)' ,5X,'J',iX,'M«C(I , J) • ,4X, 'HU,J>«/T<,9,'(10**24ATOMS/CC)t ,F0RMAT(//2X,I2,3X,F9.4,2X,F9.4,<,X,'THE SAME AS REGION «tt2)FORMAT(16H-S0URCE SPECTRUM»FORMAT)//' INTEGRATED FLUX IN/CM*»2-SEC) AS A FUNCTION OF RADIUS1/l/« FLUX',12X,'VOLUME WEIGHTED1/T18, ' AVERAGE RADIUS»/T23*•(CM) • / (FORMATJ//' FLUX (N/CM**2-SEC) PFR UNÎT ENERGY AS A FUNCTION OF ENE1KGY IN REGION',2X,12///' FLUX',6X,•AT»,6X,•ENERGY EBAfi IN WFV'/IF0RMAT(26I3 iF0RMATU0I2)F0RMAT<F10.5,F9.T,5I3)FORMAT(8F10.5IFORMAT»1QF8.4)FORMAT!I3.F8.6.E14.7!FORMAT (1 1F7.<»)FQkMAT)S< I 3,f- 11.9) )FORMAT(20A4IFORMAT(9A4,I2,F1O.5,F14.71F9.5,F9.7»F 0 R M A T ( / / 2 X , l 2 , J X , f S . 4 , 2 X , F 9 . 4 , 4 X , ' l ' . 5 X , I 3 , 5 X , F 1 1 . 9 )F O R M A T ( T 3 U I 2 , T 3 8 , 1 3 , T 4 6 , F 1 1 . 9 IF Q R M A T ( 4 ) I 3 , ' , ' , 3 X , F 1 0 . 5 , 4 X I )F O R M A T ( • • • » 2 X , F 9 . 5 t 9 ( 3 X , F 9 . 5 ) lF O R M A T ( i H t . 7 , f a x , F 8 . 5 IF O R M A T ) / / ' T O T A L K I N E T I C E N E R G Y T R A N S F E R E D = ' . E 1 4 . 7 , ' W A T T S ' , / / '
1 E N E R G Y L E A V I N G r f L L T H R O U G H C E L L B O U N D A R I E S = ' , E I 4 . 7 , « W A T T S ' / / '2 E N F . R & Y E N T E R I N G C E L L T H R O U G H C E L L B O U N D A R I E S = ' . E 1 4 . 7 , ' W A T T S ' / / 1
3 T O T A L E N F R G Y L O S T T H R O U G H C E L L B O U N D A R I E S = ' , E 1 4 . 7 , ' W A T T S 1 , / / '4 T C J Î A L E N F R G Y L U S T T H R O U G H L O W E R E N E R G Y B O U N D = 1 , F 1 4 . " ' , ' W A T T S ' )
F Û K M A U / / ' T O T A L F N E H G Y I N P U T = ' , 6 1 4 . 7 , • W A T T S ' , / / 1 T O T A L F I N A L E1 N E R G Y - ' , t l 4 . 7 , ' W A T T S * , / / 1 O F W H I C H ' , F 1 4 . 7 , ' W A T T S C O M E F R O M GA2 M M A F-AY E N E R G I E S I N I N E L A S T I C 1 / / ' S C A T T E R I N G C O L L I S I O N S , A N D ' ,3 E 1 4 . 7 , ' 1 W A T T S C O M E F R P M N O N - C E N T E R - Q F - M A S S 1 / / • E N E R G Y I N A B S O P P T I O4 N R E A C T H J N J ' I
F O R M A T ) ! * » 4 A 4 , < , X , E 1 4 . 7 , 9 X , E 1 < « . 7 IF O R M A T I ltr\<*. 7 . ' W A T T S n F . R F T R A N S F E R R E D T O ' , < » A < » IF O R M A T ( / / ' T H h T O T A L K I N E T I C E N E R G Y T R A N S F f R R P O B F T W F f N R E G I O N S ' ,
I I ? , 1 A U D ' , U ' , ' I S ' , L 1 4 . 7 , « W A T T S ' )F O R M A T ) / / ' r M r ' . t , n S S S F C T i O N O Û T A I S A S F O L L O W S ' / / 7 ( I 3 , ' , ' . F 1 0 . 5 ,
1 2 X 1 1F O f M A T ! . ' / • l ' < . ' . ' ! M S I N T E G R A T I O N S P E R S E C O N D P F R M G . P E R M I N U T E O F
H k « A U ! A M U N ! ' . M l O I O N ' , ! 2 IF ( j k M A T ( / ' i t f K . l l v f F L U X = ' . F 1 4 . 7 , ' N / C M * » 2 - S F C IF O R M A T 1 * 4 4 , I 2 , F f l . 4 >F O R M A T ) ' L n w t R E N E R G Y B O U N D ( E L ( K ) ) A N D A V E R A & F N E U T R O N E N E R G Y ( E B
l A P . ( K ) ) A ! ) A F U N C T I O N 0 ? G R 0 U P ' / / 4 ( ' K ' , 4 X , ' E L ( K ) ' , 6 X , ' E f i A P ( K ) * ) / 42 ( 7 X , ' ( M f V I ' , if,,' I M h V ) ' , I X ) )
F C ' R K A T C t ( I 1 . 2 X , F H . ' . , 2 x , F d . 4 , 2 X l )F O R M A T ) • » l H O A B S u R P T I L i N C R O S S S E C T I O N S F O R u 4 1 4 / / 1 0 M K ' , 9 X ! )F U R M A T ) 1 0 1 1 H . F 9 . 5 ) )F O R M A T ( 3 9 H C E L A S T K S C A T T E R I N G C R O S S S E C T I 0 N 5 F O R , 4 A 4 / / 1 O ( I K « , 9 X
1 ) )F O R M A T C - l H ^ l N t L A b T I C S C A T T E R I N G C R O S S S E C T I O N S F D R , < 1 A 4 / / 1 P ( 1 K ' ,
1 9 X ) I
F O R M A T ( b O H O A V F K A G E G A M M A E N E R G Y I N I N E L A S T I C C O L L I S I O N W I T H , 4 A < t / /
1 1 0 ) ' K * , 9 X ) IF O R M A T ( 3 3 H O I N E L A S T I C S C A T T E R I N G K A T P I x F O B , A A A )F O R M A T 1 l l H C F ^ O M G P O U P , I 3 , L 1 H T O G R O U P K / / 1 0 ) ' K e , 9 X I )
-30-
Ob J5
O-i i 70533
0*i 39
43 F 0 R M A T U 5 H C M A T E P IALS IN THE P E A C T O R / / ' M A T E R I A L « , 5 X , « R E F . N 0 . ' , 4 X1 , ' M A S S ' , 5 X . ' A L P H A ' , 6 X , • C S I « / T 1 7 , • I M P R ) « T 2 7 , • ( A M U ) ' / / I
4* FCRMAT ft A*. , 1 X , I 3 , 3 X » F 9 . 4 , 2 X , F 8 . 5 . 2 X , F 8 . 5 >4 5 FORHATl 1 Û U 3 , 9 X i I4 6 FORMAT!/. ' . X . 2 0 A 4 )47 FCRMATU/' FLUX <N/CM**2-S EC ) PER UNIT LETHARGY AS A FUNCTION OF E
1NERGY IN REGION',2X,t2///« FLUX',6X ,• AT • ,6X ,'ENERGY E8&R IN M E V / >48 F0RMAf(//« AVf-'AGE FLUX ! N/CM**2-SEC > PER UNIT ENERGY, WEIGHTED BY
1 •,4A4///' FLUX' ,6X,«AT1,6X,«ENERGY EBAR IN M E V / I49 FÙRMAT1////1 KINETIC ENERGY TRANSFERRED IN REGION •, 12//• MATERIAL
I'ilOX,21'ENERGY TRANSFERRED'tSXl/TZSi'lWATTS/GRAMt'fTABt'fWATSl'/l51 FORMAT(E14.7)50 FORMAT!//' THE FOLLOWING DATA IS NORMALIZED TO ',E14.7,' K W A T T S V
1 OF U235 FISSION ENERGY PRODUCED PER CM THICKNESS OF LATTICE CELL'21END
\
000100020003
00040005000600070008000900100011001200130014001500160017001800190020002100220023002^002500 26
002 7002 8
00290030003100320033003*0035003600370038003900400041004200430044004500460047004800490050C051005200530054
220
221
219
210218
SUBROUTINt KAVtNi»<N,K,KIN,EN»COMMON/ALL/OPT ION(40 I , V H 0 I ,QF ( 30 )C0MMÛN/RâV/VK(60l,UV(60 > tL IKE(30 I,JL(30>,MPC(30,20 I , n N S ( VIS I GIN!1300 I,S IGEI 20,60) , E.9ARI60),EGAHA(20,60 I,SDOJ< 30,20),ZPH1(30,601,ALPHAJ20),AMASS(2OI,S!GI(2O,fcOI,CS!(20;DIMENSION RK. ( 60 ( , ARK I 60 I , Q< 30, 60 IINTEGER*? OPTIONRKUi=VMK)APK(1I=UV(KIKM = K.-200 220 KP=1,KMKMI=K-KPRK (KP+1 I=RK.( KP(*VK (KM1 »ARKIKP+1I = ARK(KPI*UV(KM1)DO 203 1=1,N0F(U=0.DO 221 KP»1,K.M
0(1,KP)=O.MAX=JL<1IDO 201 J=1,HAXMP=MfiC(I,J)If (MP.rjT.3OOI MP = MP-300
TO 201TO 210
212
214
21 o
215
GOGO
I ) 1
If(MP.Gr.2OO)I M M P . G T . 1 0 0 iAL=ALPHA(MP)IF ( ( RK(K-1 I*AL I .GT.RKU ) ) GO TO 21BIF< (RK.(K-1 >*AL).LT, 1. ) GO TO 2190F(II=OF!I)KRK(l) PK(K-1)-AL*( l.*ARK( 1I-ARK1K-1 I-6L0G (
1SDGJ< I,J)/(CSHMP)»(1.-AL)IGO TO 216QF(M.«OF(I)t((RK(l )-l. )/«K(K-l »-AL*ABK(l) )«SDOJ(I ,J> /(CS1(«P )•(!.
1AL! 1GO TO 218HP=MP-10QIMLIKEI I ).NE.O) GO TO 213AL=ALPHA(MP)A=AMASS(MP)AM=(A*A*1.)/((A*l.)*lA+l.)iAN»A/JA*l.>DO 202 KP=l,KMKM1=K-KPIF ( (MP.C( I , J I ,GT» 100) .AND. iMPC( I , JI.L1.200) I GO TO 211IF((MRCII,J).LT.3OO).OR.(K.GT.KIN)) GO TO 212
0 ( I , K P I = U ( I , K P ) + D E N S ( I , J ) * S I G I N ( K X )I F ( ( R K ( K P ) * A L I . G T . R K l 1 ) ) GO TO 211P R = S I G E | M P , K M 1 ) * D £ N S ( I , J ) / ( U V ( K M l ) * ( l . - A L I II F ( ( R K ( K P f l ) * A L ) . G E . l . ) GO TO 2 1 40 ( I , K P > = 0 ( I , K P ) + I R K ( l ) - l . ) * ( K - / R K ( K P ) - l . / R
GO TO 2 1 1I F ( ( R K ( K P ) * A l l . L T . l ) GO T O 2 1 5I F ( ( R K l 1 I ) , G T . ( R K ( K P + 1 ) * A L ) ) GO T O 2 1 6O < I , K P ) « 0 ( I f K P ) + P R * ( R K ( l ) / R K ( K P ) - A L « ( I . • ARK ( 1 ) - A L O G < A D - A R K ( K P 1 1 )GU T O 2 1 10( I ,KP)=O( I , K P ) + P R * ( R K m » U . / R M K P ) - l . / R M K P + l l ) - A L * U V I K M l » lGO TO 2 1 1I K « R K ( K P + U * A L ) . L T . R K « 1 > ) GO TO 2 1 7Q ( I , K P ) = Q ( I , K P ) + P R * ( ( R K ( l l - l . ) / R K l K P ) - A L * A R K ( l ) )
- 82 -
00550056
00570058005900600061006200630064006500660067006800690070
217
211
202201
213204223
203
GO TO 2 1 10( I ,KP)=Q( I , K P | * P R * < ( R M 1 I * I 1 . / R M K P ) - 1 . / R K ( K I > * L > ) >- l . /RK U P
l l . - A R M K P * l >-ALOG(AL ) MVKN=<AM«EBAR<KM1 )-AN*EGAMAIMP,KM1»1/ENÏ F ( V K N . G E . R M l ) IG0 TO 202I F i V K N . G E . l . ) Q ( I t KP» = Q I I , K P | * S I G I I M P , K H l » * O E N S I I t J ICONTINUECONTINUEGO TO 223DO 204 KP=1,KMQ ( I , K P ) = Q ( L 1 K E ( I I ,KP)DO 203 KP=l ,KMKM1=K-KPO." in = QFJ I ) * 0 ( I , K P ) * P H N I , K M 1 ) * V ( I ICONTINUERETURNEND
-83-
000100020003
0004000500060007000800090010001100120013001*.0015001600170018001900200021002200230024002500260027002800290030003100320033003*00350036003700380039004000410042004300440045004600470046004900500051005200530054005500560057
310
3! I
320
SUBROUTINE L E N O R E < N , C C J , H O P E « K ICOMMON/ALL/OPT I ON U O ) , V( 3 0 > , OF < 3 0 )C O M M O N / L E N / R 1 3 0 » , S ( 3 O | , T i 3 O > , J J ( 2 , 3 O ) , H V V ( 3 0 ) , W O V i 3 0 ) , w I V < 3 0 ) i
1 S T 1 3 0 . 6 0 )0 1 MENS ION A ( 3 0 ) , B ( 3 0 ) , C ( 3 0 ) , D ( 3 0 )R E A L » * J JC < N * 1 t = » C O JD ( N « - l > = 0 .DO 3 0 0 I ! = 1 , N1 = N - I 1 + 1
I F ( I . E O . l ) GO TO 3 0 1TH = R ( I l - R ( I - l )X = S T ( I , K ) * T HY « R ( S - U / R I I IAVL = 4 . « S T ( 1 , K ) * V ( I I / S f I II F ( S T ( I t K ) . L T . 1 . ) GO TO 3 1 1I F < ( S T ( I , K I « R ( J ) ) . L T . 4 . ) GO TD 3 1 1G = 2 . * S T I I , K ) * S O R T ( 2 . * R ( 1 ) * T H )1NTEGER*2 OPTIONP - 4 . * G » 2 1 .
P = ( 1 . * 3 O . 7 5 / I P * P ) ) / S Q R T 1 P )
PC0=3.*(l.-4.2554*EXPl-C)*OI/(1IF1X.LT.4.I GO TO 310POI=.OO552?*EXP(1.14*I4.-X))»SQRTIY)PIO=PQI/VPOV=1.-POI-POOPIV=l.-P10PVI=Y»PIV/AVLPVO*POV/AVLPVV=1.-PVI-PVOGO TO 320CALL HOPE(X.Y.PVI,PVB)PIV=AVL*PVI/YP I O = 1 , - P I VPC) I =Y*P 10
PVO=POV/AVLPVV»I.-PVI-PVOGC TO 320C A L L H O P E ( X , Y . P V 1 , P V O )PVVM.-PVI-PVOPCV=PVO*AVLPIV=PV1*AVL/YPI 0=1.-PI VPOI=Y»PIOPOO=1.-POI-POVZ=l./(l.-T(I)*PVV»ZL = l.-Ml.-.75*Tm
WVV( I ) = P V V ZDA=10.*(.15-P10)DB=10.*(PI0-.05)IF(DB.GT.O.I GO TO 321H O V d ) = tl.-2.*P0I )*ZLWCI=P01•!.5»P0V*T(I)*POI«ZL
-84-
005800590060006100620063006*006500660067006800690070007100720073007^ÛC75007600770C780079008000810Q820083008*0035008600870088008900900091009200930094009500960097009800990100OlOi01020103010*010501060107oioa01090110OUI01120113Oil*0115
>*ZLWlVlI > = (l.-?.*PIO»*ZL
321
322
301
312
313
323
32*
Ml 1=.25*PIV*T(I)«ZLGC TO 302IFIDA.GT.O.) GO TO 322MOVU >=POV*ZW01=P0I+P0V*PVI*TU )*ZWOO=P00*P0V*PVO*T(I)*lMlV(I)=PIV*ZWIO=PIO*P!V*PVn*T(I)*ZMII=PIV*PVI»TlI)*ZGD TO 302MOVU)=DB*POV*Z*DA*(1.-2.«POII*ZMOI=POI+POV*T(I)*(DB»PVI*Z»DA*1.5*P0I*ZLMO0=POO»POV*T(I)»(DB*PVO*Z*DA«.25*ZLIWIVII)=DB*PIV*Z+DA*(l.-2.*PI0)*ZL
HII=PIV»T(II*(DB*PV1«Z*,Z5*DA*ZL)GC TO 302X= .T»1 ,K)*R( 1 )V = 0.
IF(X.GT,4. ) GO TO 312CALL riOPE(X,Y,PVI,PVOIPVV=1.-PVOPOV=AVL«PVOPCO=1.-POVGD TO 313P00=.125/1STlitK)*ST(1,K»*RI1)*R(1J)PCV=l.-POOPVO=POV/AVLPVV=1.-PVOPV1=O.PIV=O.PIU=O.POI=0.Z=l./(1.-T(l)*PVV)ZL=l./(l.-T(l)*PVV)wvr=pvi«zHVO=PVO*ZWVV<1)=PVV*ZMOI=O.WIV(1!=O,WIO=>O.WII*O.DA = 10.*U2-PVOIDB»10.*(PVO-.1IIFIDA.GT.O. ) GO TO 323WDV«H=POV*Z
GO TO 302IFtDB.GT.O.» GO TO 32*WQVIII»POV*ZL
GO TO 302MOV(II=>POV«<OB*Z*DA*ZL)
-85-
01160117011801190120012101220123
01250126012701280129
302 DEN=L./(l.-M00*C(I*llIIF(I.EQ.l) GO TO 300A(I)=WI0*06NB< I»=WOO»DCm>WII»MQI*C(I*ll*A(ItD(1)=WOI*(C(
300 CONTINUEJJ(Z,1)=(WOO*D(2JJ(1,1)=C(2I*JJ(2,1)*D(2)DO 303 1=2,NJJ(2i I)=A< I J*JJ(2,I-IKBUI
303 J J d . I 1 = C*RETURNEND
II*DEN
-86-
0001000200030004000500060007
oooe00090010ooii001200130014001500160017001800190020002100220023002400250026002700280029003000310032
400
401
402
404405
SUBROUTINE HOPE!XCY,P,Q)IFU.EQ.O. 1 GO TÔ 400ÏF1X.LT.1.» GO TO 401E=EXP(-X>
G=4.*X*13.GZ=(.5-E*SQRT(2.54647/G)»<Gl = l.5-E*(i.*3.08/<F*FM/F>/XH=1./»X*X)SZ=((<(-.12032*H*.26569)«H-.GO TO 402GZ=.63662
. 75/(G*GM
-.19625I«H*1 2*X)
GO TO 402A=ALOG(XIXX=X*XGZ=.6 3662-.5*X*.106l*XX*(1.94926-A)•.00265*XX*XX*t1,89926-A>Gl = l.«-.5*X*U-.9228)-.1660*XX*.0177«X*XXSZ=1.-1.3333 33*X-XX*« i.0 3243»XX*.49872I*A-,05505*XX-,68542»IH (Y.EQ.O. ).0R. (Y.EQ.l.M GO TO 404ALAM=i(SUKT(l.-Y*Y|»ARSlN(YI/Y-1.5708*YI/(1.-Y 1-2. )*.87597GO TO 405ALAM=YANU*l.8*.3/<(1.01-Yl*(l.*4.*XI)ALPH«Y-JY-ALAMI*EXP(-ANU*X»P=((l.-ALPH)*GZ*ALPH*Gl)*Y/(1.*Y)YBAR=1.-YAL=Y»YBAR*t6.*X-3.)/(2.*X*l.)O=((Y8AR-ALJ*SZ*Y*G1)/(l.-AL)-°RETURNEND
APPENDIX
SAMPLE OUTPUT FROM NEVEMOR
NEVEMGR
51 GROUP ENERGY DATA FDR NINE MATERIALS INCLUDING INELASTIC MATIX FOR U23P
ENERGY CEPENDENT INPUT DATA
LCWER
K
159
13172125293337414549
ENERGY
ELCKI( PEVI
10.00006.9C004.8C0 03.3C002.3COÛ1.60001. 10000.76000.525C0.36000.25)00.17500.1200
BOUND (ELiK
E9ÛRJK)(MEV)
7.24445.02173.44782.39861.67391.14930.79450.54960.37970.26230.1B240.1261
) ) AND
K
26
10141821263034384246 .50
AVERAGE
ELIKI(MEV)9. 10006.30004.35003.00002.10001.45001.00000.69000.48000.33000.23000.16000.1100
N E U T R O N
F B A R (I M E V
9.54306.59554.57133.14762.19851.52381.04920.72440.5C220.344B0.23990.16740.1149
ENERGY
K| K1
37
1115192327313 D
39434751
(FBAR (K) |
EL(KI( HE V I8.30005.75004.00002.75001.90001.32500.91000.63000.43500.30000.21000.14500.1000
AS A FUNC
EB4R(K(MEV)
8.69396.02084.17^62.873?1.99831.39660.95430,65950.45713.31480.2',9R0.15240.1049
TION
1 K
48
12162024283236404448
OF GROUP
FL(K)MEV)7.60005,25003.60002.50001.75001.2000o. moo0.57500,40000.27500. 19000.13?5
753•j
11P000,00
FBAR(K)(MFV)
, 9 4 4 9. 4 9 b ?. 7 9 6 5. 6 2 3 0« B 2 4 0. 2 6 1 5. B6 94o6021.417^*. ? 8 7 ?.1998. Î 3 fl 7
CROSS SECTION OATA AS A FUNCTION OF GROUP
ABSOKPTIGN CROSS SECTIONS FOR ALUMINUM
K1
1121314 151
0 . 00 . 00 . 00 . 00 . 00 . 0
K2
1222324 2
0 . 00 . 00 . 00 . 00 . 0
K3
13233343
0 . 00 . 00 . 00 . 00 . 0
K4
14243 44 4
0 .0 .0 .0 .0 .
0 '0000
K
515253545
0 . 00 . 00 . 00 . 00 . 0
K6
1626364 6
0 .0 .0 .0 .0 .
0000
K7
17273 74 7
0 . 00 . 00 . 00 . 00 . 0
K8
1828384 8
o.c0 . 00 . 00 . 00 . 0
K9
1 92 93<54 9
0 . 00 . 00 . 00 . 0C.O
K10203 0^ 050
0 . 00 . 00 . 00 , 00 . 0
ELASTIC SCATTERING CROSS SECTIONS FOR ALUMINUM
K1
112 13 14 151
O.231CO1.004501.827002.533002.205003.55200
K2
12223242
0.251601.092001.385002.227252.98650
K3
1323334 3
0.262501.210001.947003.100003.31200
K4
142 43 44 4
0.313201.416001.902752.623504.65000
K
515253 545
0.361001.616502.025003.300003.27250
K6
162 63 64 6
0.409501.666002.115003.825006.11000
K7
172 73 74 7
0 .1 .2 .3 .9 .
4600068150016006700045000
K8
1828384 8
0 .U2.?,5o
56700710C0346002620070000
K
i -
2 93 94 9
0.68200I.7«i?753.074003.71700?.09000
K1020304 050
0.860?51.7B1252.409004O 0 94T02.433^0
1KELASTIC SCATTERING CROSS SECTIONS FOR ALUMINUM
CO1
1112131415 1
1.000000.690000.130000 . 00 . 00 . 0
212Zl3242
AVERAGE GAMMA
K1
1121314 151
7.000001.950001.100000 . 00 . 00 . 0
K2
1222324 2
0.990000.650000.100000 . 00 . 0
ENERGY IS
6.400001.600001.100000 . 00 . 0
31323334 3
0 .0 .0 .0 .0 .
97000590000500000
414243 44 4
0.940000.530300.ClOOO0 . 0O.C
INELASTIC COLLISION WITH
ft3
1323334 3
5.1 .1 .0 .0 .
65000300001000000
K4
14243 44 4
5.150001.150001.100000 . 00 . 0
•s1525354 5
K5
15253545
0.920000.470000 . 00 . 00 . 0
ALUMINUM
4.600001.100000 . 00 . 00 . 0
616263 64 6
K6
16263 64 6
0.880000.400000 . 00 . 00 . 0
4.100001.100000 . 00 . 00 . 0
71727374 7
K7
1727374 7
0 .0 .0 .0 .0 .
3.1 .0 .0 .0 .
8500033010000
6000010000000
8
18283 84 8
K8
192B1 94 8
0,810000,280900 . 0o.r0 . 0
3,150001.100000 . 00 . 00 . 0
919? 9394 9
KQ
1 92 9" \94 9
0,78000C.22COO0 . 0C.O0 . 0
2.75000U100000 . 0C . O0 . 0
1020i n4 05 0
K1020304 P
5 Û
0,73000C.1RCOO0 . 00 , 00 , 0
2,300001, 1 00rn0 , 0runO.P
AflSGRPTICN CROSS SECTIONS FOR CAR3ON
K1
u2131M51
O.13O0O0.00.00.00.00.0
K212223242
0.jdOOD0.00.00.00.0
ELASTIC SCATTERING CPOSS
K1
1121314151
0.4000C1.842751.846322.935943.827824,37663
K212223242
0.431602.244001.961403.033243.38846
K3
13233343
0.035000.00.00,00.0
K4
14243444
SECTIONS FOH
K313233343
0.436242.314752.0O4603.131263.93960
K4
14.243444
0.0
cec.o0.00.0
CARBON
0.760001.605402,206263,264004,00656
K5
15251545
K5
15253545
0.00.00.00.00.0
0.811802.458702.3150C3.316444.(16805
K6
16263t4'>
K616263646
C O0.0C O0.00.0
0.510Û01.691202.407603.393904.12141
K7
17273747
K7
17273747
C O0.00.00,00.0
Q,9lS801.57542?,549253,477544.17763
K8
18283848
K6le2flîa48
0,
n.0,n-,0,
î,1,
z,3,4.
Crc00
023C06)5??6^765578642'-576
K9
!929•»9
4 9
K.9
19293949
0.C.r.0.0.
0.1.2.3.4»
000
0
8 340 071020746456557629P40
K1020304050
K1"?.r>3o4050
0.fi.
0,
r-,0,
1,1,2.3,4,
nnn
00
1470074^ÇPliOl'?T*bC S
3 3 ? 6 C
INELASTIC SCATTERING CROSS SECTIONS FUP CARBON
K1
1121314151
0.26C000.00.00.00.00.0
K2
12223242
AVer "(JE GAMPA E
K1
1121314151
• 55000u.O0.00.00.00.0
K2
12223242
0.120000.00.00.00.0
NERGï IÎM
4.430000.00.00.00.3
K3
13233343
0.300000.00.00.00.0
K4
14243444
0.43500C Oco0.00.0
INELASTIC COLLISION KITH
K3
13233343
4.430000.00.00.00,0
K'414243444
4.43000O.C0.00.0O.C
K5
15253545
C
K5
15253545
0.0.0.0.0.
245000000
ARBON
4.0.0.0.0.
430000000
K6
16263646
K6
16263646
C.270000.00.00.00.0
4.430000.00.00.00.0
K7
1727M47
K7
17273747
0.Z30000.00,00,00,0
4.430000,00.00,00,0
KP
18?8IP48
KA
182818
0.100000.00.0O.P0,0
4-430000,00.00.00.0
K9
1929
3949
K"5
n293949
0.0,0.0.n.
4.Co
04000000n
4 ~<.r o 00
0.0p ,
a.n0
K10? 0• o
4050
K1C20304PR P
C0,0,0,
c
0,
c0.0.0.
000o0
000
n0
ABSORPTION
K1
1121314151
0.0.0.0.0.0.
000000
CROSS SECTIONS FOR DEUTERIUM
K212223242
0.0.0.0.0.
ELASTIC SCATTERING
K1
11213141SI
0.1.2.3.3.3.
600006600069000110002900C39000
K212223242
1.1.2.3.i.
0
a000
CROSS
1000096000750001400030000
K3
13233343
0.00.00.00.00.0
K4
14243444
SECTIONS FOR
K3
13233343
1.180002.080002.830003.160003.30000
K4
14243444
0.0.0.0.0.
00000
K5
15253545
DEUTERJUM
1.2.2.31.3.
2500015000850001800030000
K5
15253545
0.0.0.0.0.
1.2.2.3.3.
00000
3200025000900002000032000
K6
16263646
K6
16263646
0.00.00.00.00.0
1.420002.350002.930003. 200.503.31000
K7
1727}747
K717273747
0.00.0O.C0.00.0
1.500002.430002.980003.220003.35000
K
aîfl28
48
K8
182B3941
0.00.00.00,00.0
1.600002,510003,0?0P03,240003. if-rnc
Ko
19293949
K9
19293949
0.00.00.00.00.0
1.690002.SP0O03.950003.2TC003. ?=?noo
K10203040•>0
K10203040SO
0.00,00.00,00.0
1.7 80C0?,6ïoon3.0P0003., 2 W i O3,3300"
^ELASTIC SCATTERING CROSS SECTIONS FOR DEUTERIUM
K1
1121314151
0.00.00.00.00.00.0
AVERAGE
K1
1121314151
0.00.00.0o.ô0.00.0
K2
12223242
GAMMA
K212223?42
0.00.00.00.00.0
ENERGY
0.00.00.00.00.0
K3
13233343
0.00.00.00.00.0
IN INELASTIC
K313233343
0.00.00.00.00.0
K4
14243444
0.00.00.00.00.0
COLLISION
K4
14243444
0.00.0O.C0.00.0
K5
15253545
HITH
K5
15253545
0.00.00.00.00.0
DEUTERIUM
0.00.00.00.00.0
K6
16263646
K6
16263646
0.00.00.00.0O.û
0.00.00.00.00.0
K717273747
K7
17273747
0.00.00.00.00.0
0.00.0O.O0.00.0
KBIS•>H
3&46
Kfl
182838'.H
0.00.00,00.00.0
0.00,0
o.n0,00.0
KQ
19?9394<?
K9
19293949
O.C0.00.00.00.0
0.00.00.00.00.0
K10?0304050
K10?0304050
0.00,00.00,0
o.n
0.00.00.00.00,0
IO
ABSORPTION 1
K1
1121314151
0.00.00.00.00.00.0
:ROSS SECTIONS I
K212223242
0.00.00.00.00.0
K3
u233343
-0« HYDROGEN
0.00.00.00.00.0
K414243444
ELASTIC SCATTERING CROSS SECTIONS FOR
K1
1121314151
0.470001.310003.150005.250008.5000012.500G0
KZ122231'42
0.980001.920003.J50005.500008.9OCOO
K313233343
ifccLHSTIC SCATTERING CROSS
K11121314151
0.00.00.00.00.00.0
K212223242
0.00.00.00.00.0
AVERAGE GAMMA ENERGY IN
K11121314151
0.00.0G.O0.00.00.0
K212223242
0.00.00.00.00.0
K3
13233343
1.055002.O5OOO3.500005.800009.20000
SECTIONS
0.00.00.00.00.0
K414243444
FOR
K4142434
1
C O0.0
o.c0.00.0
HYDROGEN
1.14C002.130003.750006.100009.70000
K515253545
K5
15253545
HYDROGEN
0.00,00.00.00.0
INELASTIC COLLISION HlTf
K.3
13233343
0.00.00.00.00.0
• K
14243444
0.00.00.00.00.0
K5
15253545
0.00.00.00.00.0
1.220002.320003.900006.40000
10.00000-
0.00.00.00,,00.0
1 HYDROGFN
K5
15253545
0.00.00.00.00.0
K616263646
K6162b3646
K6
162636"b
K616263646
0.0.0.0.0.
1.2.4.6.
10.
0.0.0.0.0.
0.0.0.0.0.
.0,0,0,0,0
3100045000loono7000040000
00000
00000
K717273747
K7
17273747
K7
17273747
K7
17273747
00,00,0,
1,2,4,7,
10,
0.0.0,0.0.
0.0.0.
a.0.
.0
.0
.0
.0
.0
.40000
.58000,30000.00000. BOOOO
.0,0.0.0,0
00000
K8
18253R49
K8
m21384fl
KB
19293H43
K
1826384*
0,0,0,0,0,
I»2.4,7.
1 1.
0.0.0.0»0»
0.0.0.0.0.
.0
.0
.0
.0
.0
.52OPO,70000,^500040000,30000
00
c00
00n0n
K9
19213949
Kc>
192e)3949
K9
19293949
K9
19293949
0
00,0.
1,2,4,
7.1 1.
0.0.0.0.0.
0.0.0.0.0.
.0
.0
.0
.0
.0
.6J000
.88000
.75000
.BOOOO,60 000
,0,0,0,00
00000
K1020304050
K102010'.050
KIC20304050
K1020304050
00000
135fl,
12,
0,0«0«0.0,
0.0.0,
n.c,
.0
.0
.0
.0
.0
,7?ono•nsnoo. oono»toono.noon
>o
• n,0,0
000n0
I—1
I
ABSORPTION CROSS SECTIONS FOR IRON
K1
112131415.1
0.0.0.0.0.0.
000000
K2
12223242
0.0.0.0.0.
001000000
K3
13233343
00000
.0
.0
.0
.0
.0
K4
142434
44
0.0.0.0.0.
00 ,000
K515253545
0.0.0.0.0.
00000
K6
16263646
0,00.00.00.00.0
K7
17273747
0.0.0.0.0.
00000
Kfi
IH
384H
0.0.0»0.0.
0
00p
KQ
1929394<3
P.0.0.0.0.
000
o0
K10?0104050
0.0 .
0.0.0.
00000
ELASTIC SCATTERING CROSS SECTIONS FOR IROK
K1
112131
51
K
0.26520 20.88000 121.650C0 221.89000 321.98875 <>23.31200
K0.31320 30.93240 131.71000 231.92000 33?.T75OC 43
K0.35720 4i.Il 390 141.69600 242.16000 342.60400 44
C. 40200 51.I96JQ 151.86430 252.531-30 354.488J0 45
K0.44520 6l.?4 740 S 61.41C0O 262.97500 361.410CC 4*>
K0.51293 71.42730 171.6500G 273.65400 372. 7<-050 47
K0.57750 P1.44300 131.39500 ?fl
3.32SC0
KO..6*IPO «1.5400 0 19l.o 7^P0 ? 91 . P t 5 ? 5 ""3
0.70500 101.7? ?n
1 •» î. •=• )
INELASTIC SCATTERING CROSS SECTIONS FOR IRON
11121314151
1.400001.450000.580CO0.00.00.0
212223242
1.400001.400000.510000.00.0
313233343
1.390001.100000.4 70000.00.0
414243444
1.380001.020000.400000.0
o.c
515253545
1.3 7OOC0.810000,46000O.CC.O
6
162!:364 6
l.360000.900000.3S000O.ÛC.O
7172 73747
1.36000,7.890000.21COO0.00.0
31928
1.350000.P500ÛO.O^OPO0.00.0
q
19293949
I.34000P.6 7P00o.Or.or.o
10?Q(04T
50
11, 3P0<" 0O.ftlOCC0.00.00.0
AVERAGE GAKPA FNERGY IN INELASTIC COLLISION WITH
K1
1121314151
8.600012.35C0O0.845000.00.00.0
K212223242
8.000001.950000.845000.00.0
K313233343
7.450001.55CC00.845000.00.0
K414243444
6.750001.300000.84500O.CC.O
15253545
6. 10000l.OPOOO0.S45000.00.0
K6
16263646
5.450000.96O00C.845000.00.0
K7
17273747
4.8000C0.855900. 845000.00.0
Kfl
l*2fl3P
4.150P0
o.a'^o0.84SCO0.00.0
K,
919293944
?.0.0.0.0.
6"C(84e'0
00
10 ?Cir
•iO
2- «350"n
0.00.00.0
coo
oo
* o« 4
oco^
«c o-
ocor a i
oo
ooooo
ooi ra-—
o
o
o00
oo
oM
O
o
a—'
oo
a:
oo
- i
o
o
•cI -
1
o
oc
om
C
o
rg
O
o
0PA J
O
o
I M
O
o
rg
o
oo
o
o
o
am
co
m
O
o
oo
O
o
o
oirv
oc
oo
CO«^
oo
oo
i l• »
o
, - t
a:
o
•J
r.0
L.D-
C '
V rr
o.0
°
co0-
^)
c
^ -C
o
I fir
c
-
Q
Oi rrr,
tr
~
g
- >
^ j
O
-
CE—*
i!o
oCLi n•Dco
O
-0
0D
C71
r.
oc
^
„I M
C-Jcer*c
C
>t
%
" •
rM
u-r-
cr
" • »
o
cf ~
•c
C)
C ltu
i ^
* - •
0'
• *
O
?
r
c-r~Ou ^
-
•L.
h -
cc
oI Aac
r-
J
CL
Oi n
c-
r"
U"•OOcr
o
c c r o c c. c c c. c
C O O O C C C O C- Ô
c c. C c c
ff ? tr,_ rg r
c o c» c- o LJ o o o c
c o r- r o o c- r' o c.
C O C O O O O C1 O O
o o o e o o r o o o
— r\i n-. j
COO
c c o c o
o c o c- c-
c oo oo c
- - O O O O u. — Ci Ci O O• • e * * '_^ f • • • •
O O O O O u C ^ * " O O Ci O C" > C• O •"> C îJ
O 0 0 0 0 0 2 - 0 C C>TJ N O O n r i t r: •— OO 2 T 0 " t ? " 0 O > û O ' — ' J I O
fM O O ^ O O in p« Oii O J _•< (ij û U CJ O J2 i - ^ o O O t j
O O O O O « O ~* f f"1 O CJ O »_- C' — ii O U O O
a. —*#•*•*< se W - : «f •,' u i t - i -r >t -J i -j ^ -J- * *J -T •»•
i-4rsir^->r a: -vr^ ^ j u. — r r ,j _j H N I ^ jO ^u. " j iT> O J^ O L/I O - <•''
O « t o ^ ^ 0 i— *i o O O ^•— » * • É • J * * « « •H Of^"Mnj-5- ai O O O O O
i/i ^ r*i n i n ^ " ^ t/i ^ m pi n-, m m
oo a o -r CJo 'J* O O — Of -G vi- J-- > f -if « r *•* n o o r - N
* • — , . » • t -I»%! ^ a. O O O O C • ^ »?
O O < Q O O 4 Ç . I O . / Ï O X C-*r o o u r " • •© ^ o o -saLJ O O t/> o •» r- i» r*-, cJ *_J O O O»4 O V ( O i B ï l N ^ O « O O* - mooooo o ^ > ^ <r N ^ - î — •* o o »"3 o o -*J ra. • • • • • » « » • • • • * ^ . • * • • t j> ,QC OOOOOO h- O'-*|MfKJ-t'*1 < O O Û O O O -f -OO s/1 - * *I/) <f IU u»
> -
°aa
di-
UJ
00
0
IM•
O
rooo
«M
O
O
•O
m
LO00
o
o
o
a
m
O
o
o
ô
£!
oo
o
o
3
o
o
ABSORPTICN CROSS SECTIONS FOR URANIUM 233
1u21314151
211112,
•590C0.23000.37000•3500C.65000.26000
212223242
211I1
.61000
.2 5000
.37000
.39000
.70000
313233343
211,1.1,
.60000
.2 7000
.37000
.40000
.76000
414243444
ELASTIC SCATTERING CROSS SECTIONS FOR
K1
1121314151
0.1.1,2.5,8,
.62055,05558.75338.85750,71285,24320
K212223242
0,1,1,3,5,
INELASTIC SCATTER
K1
11ai314151
0.2.1.1.0.0.
,21000,05000, 60COO,06000700CO32C00
K
z12223242
0.2,1.1.0.
•61035.16145.77080.11125,94960
K313233343
ING CROSS
.24000,05000,50000,32000,66000
AVERAGE GAMNA ENERGY IN
K1
1121314151
9.3.1.0.0.0.
600012500013C0025COO0fc500038C0
K212223242
8.3.1.0.0.
510011000001000210000620C
K313233343
0,1.1.3.6.
,61440,34100,80500,33630,30360
SECTIONS
0.2.1.1.0.
3000004000,4500000000620C0
K414243444
FOP
K414243444
21111,
.40000
.31000
.36000
.41,000
.84000
URAMU* ;
0,1.1,3.6.
.64320
.55008,85652.59840,59650
515253545
?35
X5
15253545
2.1.1.I.1.
0.I.1.3.6.
URANIUM 235
0.2.1.C.0.
,50030,00000,37030,«59030,56000
INELA5TIC COLLISION HITI-
K313233343
7.2.0.0.0.
6000080000910001700005800
K414243444
7.2.0.0.0.
0000050000
eiooo14010C560O
K515253545
0.1.1.0.0.
,11000,33000,350004300087000
6867672327936558394091120
800009700033O0C9700056000
' UKANIUH ?
Kc
15253545
b.2.0.0.0.
3500C2500071000115000K 1 nO
616263646
Kt16263646
K61626?6ut
35
K
6
16263646
11111
01247
111rc
5,2,0,0,0,
.88000
.35000
.32000
.46000
.91000
.72038
.80525
.03970
.10755
.13090
rl2000.9 5000.30000.94000.5^000
. 75000
.00000
.61000
.09800
.05000
717273747
K717273747
K
717273747
„717273747
11112
01247
I1100
51000
.34000
.39000
.32000
.49000
.02000
.78925
.79340
.18400
.46400
.38720
.70000
.90000
.25000
.90000,47:?00
.20000
.80000
.51500
.06700
.04800
81628384S
K818283848
K8IB2838
Ks18283849
l.lflOOO1.3HOC01.330001.520002.07000
0.854361.801442.3*1104.781707.63875
1.950001,870001.200000.B60T00.4400C
4.7P0001.6?0000.4-^00O.OROOO0.04400
919293949
K9
192939«.9
K
919293949
K919293949
1.170001.360001.340001.540002.12000
0.921571.738002.516005.101H07.84090
2.030001.800001.150000.820000.40COO
4.250001.440000.365000.077000.04100
1020304050
K1020304050
K1020304050
K10?.r\304050
1.190001.350001.330001.S90C02.18000
0.961751.742122.654295.390958.03640
2.050001.70000I.I 30^00.760000.36000
3.900001.270000.300000.071000.04000
ABSORPriCN CROSS SECTIONS FOR URANIU» 238
1112131415 1
2.500000.580000.480000.160000.1*0000.28000
212123242
2.460000.580000.3 80000.150000.17000
313233343
2.340000.530000.24G000. 160000. 15000
4
1424344 4
2.100D00.560000.170000.17000O.lQQOa
1525354 5
1.630000.590000.210000.15000
o. nooo
162 6364 6
0 .9Q0000 ,610000.250000.140000.?noO0
71727374 7
0.630000.610000.220000,130003.21000
1»233°.4 R
0.590CO0.610000.230000.140000.?3r>00
91 929394 9
0.570000.620000.200000.140000.25000
10?0304050
0.5 80C00,590^00.17000C.140000,?60oo
t U S T I C S C A T T E R I N G C « , J S S S t C T I J N S F f i f i 2 3 R
KI
1121314 15 1
Q .
I .1 .i .£>,
1 0 .
54175103 788222355&CC7 '-J1 5 G
30400
Ki
12^i
0. 11 . 21 . •'
3 , i7. :
5 9 6 5C : 6 CC 1 2 63 1 7 5
' c< r c
K
i
1 j2 3334 3
C . 1 9 3 2 S1 . ' 0 4 8 -2 . J 1 i 7 c
4 * i 1 i 41' . - . Ï Î * 4 C
K4
i >•2 43 4
' , 4
c .1 .
4 ,
7 .
t ' I S£. '. ; i
! 04 1V Ï 4 ?
P 4 9 3
. " . 2 '• -1
i .c! i
7 c. *, i
1 72 7
12
. 82 2 35
. 60 44 2
Q
1 «•» P
- 7
- cK
10?C
6 . 4 5 3 4 0
I C • S « . F T T H ' N s f t P .; s I
K
i1121S L
4 i
5 1
0 .j .
0 .
~" J a
SJ.
5000(j00CC100 L u3r c c r cooec c
12 0 . '. •: •. . i
• • - •
0 C 0 i." C U 2
. - C l• 'Ct 1
K K
. :o os 14^ J 2 r • j 4
1 ~ . 0 i > 4I^CCi - ~ -
^ * c ,I,1 ^
' " • -
r, ; .'
K
C K ^C T 0 1 c
.- ^ . i c
, - " . • • • • *
- c . o : o :
' • , • " r •
r . - •' 7 '
71 727
0.00000
1 . 0 0 0 n '^,PC n i n••« 4 32 I
0 .0 TC0.0 00r. ion" . • < " " •
• " . 4 • • •*
-1
0n
?t ,
4
• ;
1
ï C?ci n
4 f
0 ,o.0 ,
0 ,0 ,
0<"*0
oonnon00°4 7C
Avf^âGt i . a f - i , f I N ; •-.11 , : i L L t ; i i
1t"
3<4
l11l11
4 .
1 .0 .0 .0 .
01 !>4S5& 6 1 6 2
65t 7626 1 2C1 C 4 4 R
c
*' £
32••2
J . '?
5, '1 , s
J ?tb•" G 4 6 11 7 3 4 29 9 e " - *
IBP11- 4
"i
3
J
a.i ..>.' a
»>5 7 2 2
"- 13 2 7
1 B 0 7 1•S4 7 3 0
2 1 3°2
4
1 42 4:>4
4 4
7 .3 ,
1 .- B
0 .
9 1 1 1 5134 it.2S615500041 9 g 39
c
2 e-^ c
4 e
* k n K. KT . 2 1 i r t 0 6 6.5t.7*>4 7 5 . 9 ^ 5 4 2 ? S . 4 7 ' C 3 9 c . C i r 4 5 10 4 . 5 5 2 C 3.•" . a 6 1 <"• f 1 * ? , M l ' k 17 ? . 3 P " 5 1 19 ? , l o c ? l 19 1 . ^ 1 9 0 0 PO 1 , •< 1 f> 7 91.1444J i t U 0 4 4 7 8 27 3.9=,027 ?« 0 , .•"• " 7 ? ? <3 0 . 7 9 1 ) 4 3P p . 7 2 1 - > a
16 0 . 4 15S0 37 0 . 3 7 B 0 5 1» 0 . 1 < - 3 3 3 3o " . M T - ' i 40 0 .2R6 ' l-7 0.15173 4f> n,13PO7 49 n.l?«i61 0 0.114-4
INELASTIC SCATTERING MATRIX FOR URANIUM 238
FROM GROUP
K212223242
0.00.001210.013840.014360.00501
FPCH GROUP
2
K313233343
3
TO GROUP
0.00.001200.014300.013250.00472
TO GROUP i
K
K414243444
K
0.00.002040.016810.012090.00443
K5
15253545
0.000030.002630.015250.012240.00313
K616263646
0.000050.00347C.017090.009620.00296
K7
17273747
0.0Û0060.004670.017270.010920.00280
K8
18283P4P
0.000070.006420.016860.008020.00220
«C919293949
0.0PC080,008170.015910o007880.-0207
Kin20304C•50
r0000
.00040
.00727
.01700
.00646
.00157
K11•? J
314151
C.0.0.0.0»
000700102 %01541006'îbnoi'.9
3 0.0 4 0.0 5 0.00001 6 0.00002 7 0.00003 B C.00003 9 0.0C003 10 0.00045 II P.00035 12 0.001*013 0.00150 14 0.00257 15 0.00333 16 0.00441 17 0.00604 1H 0.00836 l<? 0.01067 20 0.0OQ53 21 0.01379 22 0.01903233343
0.019B70.019130.00691
FRGM GROUP
K4
14243444
0.0C.003780.036910.028070.01051
FRCM GRCUP
K515253545
0.00.006560.052810.049440.01342
FROM GROUP
K6
16263646
0.00.011710.090970.063980.02137
243444
0.023510.017470.0C648
4 TO GROUP 1
K515253545
0.00.004920.333720.028500.00744
253545
K
K6
16263646
5 TO GROUP K
K616263646
0.00.008900.060170,039260.01279
K717273747
6 TO GROUP K
K7
17273747
0.00.018390.095810.073390.02039
K818283848
0.021430.017710.00458
0.00.006530.038070.022470.00706
0.00.013130.062510.044890.01217
0.00.026760.096260.054330.01612
263646
K7
17273747
K818283848
K919293949
0.024120.013950.00434
0.00.009050.038S80.025560.00668
0.00.018700.062210.033160.00959
0.00.035140.092790.053720.C1519
273747
K818283848
Ko
19293949
K1020304050
0.024530.O15S-50.00411
0.00.0*2600.038230.019830.00523
0.00.024270.059560.032730.00900
O.0OC730.031850. 100780.04430n.01148
28384H
K91<?293949
K!020304050
K1121314151
0.0.0.
0.0.0.0.0.
0.0.0.
c.0.
0.0.0.0.0.
024050116700322
001615036280185400489
0007002185064350269500678
0014404817092670438801089
291949
K1020304050
K1121314151
K1222324252
0.022770.011470.00302
0.000610.014440.038920.015220.00366
0.001300.032620.05891O.02"*50.00642
0.0025'.0.068370.088640.03480
304050
K1121314151
K122232425?
K1323334353
0.024^9O.CO9<,10,00226
0.00121O.O21?30,035420.015020.00344
0.002480.045930.055820.02110
0.00260C.072400.053650.0?~P6
314151
K12223242S2
K132333435^
K1424
344454
0.022160.0092B0.00213
C. 002170.029610.03314O.Oll87
0.002490.04B450.052260.01999
0.005730,086430.077790.03132
3?4252
K13?3334353
K1424344454
K.1525354555
0,0.
0,0.0.0.
0206"0P731
OC218OMCfl0306901119
0-004770.p.0.
0.0.0.0.
05769048?701867
00841079240801502235
^ • - t r in
<\j r- C f-
o «-< c o0 » o r
o o o o
CD r O CDO rr o <MO O ^ - o
• • • *o o c **.•
«M -^ r\j *rx a - rcr a; c Œ
, - | «~ Q-. (\J
9 * 0 0
C O O C
r- r- r- r- r-- - (V ^ J IT
— C 43 O"-i ,-J rr ru
o «-• o o
r* C -C- *£>•— u a rC7 f> 4j **-it*' rv P- r\.
c .- c cV t 0 f
c c c cIL ce (s a a)
a IT r\, _0 * - 4" ?Œ c r . f
0r-j j
* • (
C
o
a-
r go-
oo
or
P .
—
c
s.a
r
rZc
cri T
Occ.
c
Cr(*
0-ac
o
l-J
•£p.,gfi s
c
c.
(7
o-
I f
c
c - c c3 f * •
c c c c
r — u- A.
o — c rC C f « C
•H rg n *j
O CT- - I -^ f - oo r-ir* -H 43 a-o o a mC —i C C
« « » *•o o o o
r-4 f\l (*• ^ I
m o ••< C1
0* i-H 43 CD*-* \f\ ff\ ,-4o a1 o • *o o — o
• • * •o o o cr
: m m ro m et•-< c\j r*i •# tn
r- O O Ocr ^- -< o-4 o a **o c r o - *o o —' o
• • • •0 0 0 0
Ci
c-o
* If
o
o
IL J
CTO
O
•
a
oo°"IT
O(T
O
•
-0
CO
o
c
o
in
0-
o
o
pn
o.—1
ft
o
in ir
•J-
ot
rvj
•O
43 Œ tr OCo ^ o- —•c. M- o —^* — a: roC »-i o C
o c o c
o a- — mo o *-* o
p- tn 4;O PU ^
O O O >f0 - ^ — 0
• » * •0000
ï a. a u: x i
4 43 C*. n,a N iC rN C I ry
>« f\l m tf IT
m *r» m r.io p- œ 4;CL C7- r*- rr\
o < o o
c- r» c r
iT• tn 43C- CT -*
: o a c a cr-
ry r 0" cra J f > *j<*" f1 IT P-r\j r. j fO —' C Ce « • »
C C C O
or a a* tr cc
o «- — oo o c* c.
u- -*• cr ITt f 45 F- rf"C. O CT rrc — o o
* • • •O O O O
a
oa:
a
r -
0-
a
uatUL
of - <
> - i
ooo
i ni nooo
°
oo
f -o.0IT '
O
o
r g
•D•Ûro
°orgr gruo
oo
,1 "mopn
o oo o
CO
i n
oIMo oo o
roPO
Cl
enCM
°PO
i n•ar g
1 - 4
o
5r-IM-Ci—4
- ^
o
COIM
oa*•-*
o
p .
I Ti f '
O
o
*-«P T
i ni n
°?rvj
r-
«O
o
«
oCD<OO
o
CO
p -I MI Mt rO
o
i nO•3-•—i
oo
i n
CDp -
4-* - 4
o
°om, 4
UNO"^4
oo
i n•oo
oo
-»~Da<0CMO
O
r»
K:
aoa :
a
00
a3< j
a.
X
uau»
CO
o
ooo
o*0oo•J
o
•F-4
o
oooo
࣠O
oo
o
_^ro
oro
o
rg
_
•n
o
-M
i n
>oroO
O
orgIM
oOO
O
C^
IM
c*IM
oo o
•X. CD CD,_!
m—4
o
ro
c
o
ro
COpg
- •
o
PO
I D
r»
1 -4
o
r g
o**IM
O
00IM
^r-» -O
o
i nr~0-i n
O
IMr goo
o
oi »
«cI Mr*o
O
m
i ni nmr-oo
CO
00
i n_<oo
mmi—4
•a*•*o
o
i n
00fM- 4
r gO
o
V
«7-
IMIMO
O
CO
a.a
at -
o
a.
oot
o
us
Opr-.
ooo
o
oroOoo
to
p - l
ooo
o
adooono
si O
oo
X cr
r-•cccc
o
IN*M, - t
^0
O
C j
!M
rg•Ci noo
r g
roP_4
•o
oo
o
crIM&moo
cr
r*1 rg
>r r-—4 - *
-> o
O Ci
m ÎCO CA* ^ f*~
tr a1
•-• ^-• o
. to o
IM rg
in sf
m org rsiru JO- • O
o o
ro J-
o oIM -4rg mPO -C-• O
o o
o oPO 4>
m -tm roO •£IM r-— oO O
CF O*1
!n
m
_r".
—<oo
i n
• - 4
oo
Q
_
mr gr goo
gf
a.13Or f
a
o
oa.ouIXu.
-4 m
rg ^O CO —
• •o c
mm
roo oo o
* !H So43COP-
o oo o
•j-.
mm
o oo o
- * rg
r*Q
enO O
O O
tt O O
—' -J--» cr4—4 S /
— C• 9
0 0
m -4
r» 43in p*P- 0
*-« 0
0 0
r*1 •!"
ra f nm4 Orj mr\j in•-4 O
0 0
m «*•
•«T i n43 in<£* 4
—« r ;
0 0
m «*
o*< aom 43n*i 4?*4 O
0 0
0 0
m
! P
m
43
p»
0
0
i n
p-
.—1
O
O
0i n
a
O
0
0
—
IDOa
x( j
a
CO*n
c0
0
"»i. in
rvjf^r - «
O0
•0
0
0
0
^ IM
0
roceO*CD
C
mrg
<Jr g
CU
O
mi n000
O
0
IM
r*0
0
r g
mm0i n0
O
—t
r g
a. ^
O r-
^- D
C C
Sîm rNJC* " "
•-< in
• •0 0
•& '•t
CC 43GD i nO »4Î
rg in~- 0
O O
m .*
43 CD4 43rg m—* 0
O Ô
rr\ f
LÎ m0 043 *"•tM P*- É 0
O O
pn j -
i n
«f
m
> * •
r*as
°O»-<
pj o m ccr if. ce CL-•o o g; o1
gr rg r- *-*O -4 O O
e 9 e %O O O O
ci in mW-* *0 Oo r- cig} rg -ao ~> o
• • oo o o
r- c p-in ^- mp- r- • *•O CM J 3O — O
• I •o o o
rg C C•a o —in ci •£
c — or» e »
O O C
a. .* Cgr * —o ci mo — o
• p »O O C
CM or
o c J-4 O O
* - • • - « • • - » -
ct>t—1
CD
O
o
V CCM
CDP-
crINIO
CC
1*1
O
oC l
oC I,—i
pg
t i
. » •
-O•4-P-
O
O
oJ-
oC l
crCC
o
oPJ
co
om
•0cOOr*.o
: M cw pg egrvj !*> «f in
O tf> C f*l/\ ff1 4 (01*1 *D CO O•$" C\J P- *NO <-* O O
• • • •O O O O
(\J i . **• m
o c o c
m i»- f\i sff i IT O>\lT» J CD Nr\j r^ r- (SJO •-* O O
« 9 * mO C? O C
M r*" st tTi
_ i <*•* m
^> tsi «oO -< C
o o o
rg f\i fsi (M
Cr -O *T CM^ rg in xC- <£> <M (Mff. i \ (£ rO ^ O Ot e a *
O C O O
•4- rsj CD
F-* P- P-
O - « O
c o cC l
Pg
ir.ci n
o
Cl P"Ci J?
cr r-r-i ITr- IT-rvi c-> O
C l
m
ir.CM
1-4
a-J3O
•O
pg
•7-
r-mmo
mC l
CMp-
O
C i
CCI
p -r g— ^
m•4-
rv.CïcrJ3O
O
^.
• *
P ^
CD
Op~
c
mI T
i r
PJ
i / i
PJ.$•aso
•
o* m
p j
o•o**crc
••0
en•o
fc-
mm
C i
•atn•-
O• *
o<0
oo
J-l
gr
ITp -I T
\rO
•ai n
i n
m
o o o
cr
CD
O2
oe
opg
<r
12
H
cr
o
089C
•g-
cr
02
9«
g•r P- o p-o o ci o~rg Pg (J1 <\jD «••« O O• • n t
O O O O
£ 7 Ntfl•H| 1T' 00 PJ
pg ci cc (MO - i O O
« t »O O O O
<\j pg rg rg*vj ^ ^ m
m *J O P-J•o m o ost ci « mci rg co ryO —' O O
a • • •O O O O
m Ci ci Ci
.c in oci o cia g; PJ•T pg p-o — o
• • •o o o
rg
r-
p -
o
c
COrcipg*-4
-r g"st in
•oo•£tn
o
a3QetO
Oh-
2Ja.3OceoXuaiIL
M. CO CO• ^ pg
P- Cl
O O-4 -O—4 •—t
O —• •
o o* p- p-
-4 pg
cr p-O mci PJo oo -4
o o
x * «»•• r g
O OO r-
O coO O
• aO O
x m m<-* CM
gj sfcr mO CM
o cro oo o
«c <* *-4 PJ
tnen«p *
o oa a
O O
* CI m• * CM
CMOr-
© o9 #
o oa i NJ CM
~« CM
00 fQci gr
O f-rg p-C0 P-—t ci"H O
O O
p- r-ci gj
rg —'rg o-< crO ci— O
O O
•O -CCl gr
p.j mes pggr org gr-* oo o
in mCi gr
00 Or- gjr» Ifl-4 m1-4 O
O Ô
gr *ci gr
cr CM-H COCl P*rj m-4 O
o o
Cl Clm gr
eo ci- * O•O O
• •
o oCM IMc i gj-
*
0 .3O
gO*~
c i
0 .3OOC
19
KU
u.
ac t r cr cr crP4 N Kl 4
o r- ci cro ^ g Œ0D O CM —•^4 pg CT C i
o •-< o oo o o o
ac CD CO OO CDi-c M ct ^
eo CD J J r-m gj CM »-4cr ci PJ oo -w j -o — -• oo o o o
w p- r- i>- r--« PJ ci gr
r- o «-4 crr- cr m cio co gr -<o cr o gro o — oa a a a
O O O O
y Jl Jl t/l ^
-i CM c i gr
OOONin co r*- J3O -4 P- CMo co PJ gro o -t o
a o o o
ae in m m m-4 CM Cl J T
gr o CD c iCM - * * r>-o co o coo co rj mo o -J o• • • •
o o o o
* gr gr * • *i-4 PJ Cl g>
£$o,CM m or- CM gj
o O M o• • • •
o o o o
x m m m m-< CM en <«•
Q .
3Oceoa•-g>
a.3OacO
X
uacu.
at oCM
cocrrgCMO
o
at cr
p -j -
in
O
o
•X 03
p -
crp .
ooo
oo
ai «
C3
O
C O Offi ^ in
p-* «^ r j
o- r- Mt*. (y- rn- O O
• • •t o o
o» cr crPJ Cl J .
J3 in mHr4Ulco gj -T-> cr ci-H O O
o o o
CO 0 0 COpg ci *t
p- m in-4 m ciO g] ClMM J;M -4 O
O O O
K p- r»PJ Cl *
g» r- co— gr •»•gr p* grcr o •*•O -4 O
oôo* gj J3rj ci gr
« >4 >Wcr o g}J3 -4 mf1* ci gro — o* é 9OOO
in m mCM ci gr
- r > * •-•»•o cr uCM CM PJeo CM «
O o — O• • •
OO OO
* g* * * gr
N en *
a
oceoa*-m
a.
aceoX
aesu.
rg ci
co ** * —4CD O•M Cl
o —o o
K: o o
M0 ^
O m
o -•ô ô
je tr o- 4 CM
O P-
PJ C l- 4 - *CJ <-4
O O
X co co- J CM
m g}gj f-
o aO -4
o o
«t r- r-- ^ CM
crJ3f^co
o oo o
* g} g j•-4 CM
cror»
O O
o oM; inm
- * C M
sj* m
gT f\CP sfJ- -O00 CM
o oo c
o ogr m
- H PU
m oo mo m-4 O
O Ô
C l .»•
OD mcr PJa) r-O ClO O
ô ô
co colT| gf
co crm <t(r oN -t-J O
# •O O
p- r-Cl gr
CD <O•*• -tcr p.o <r~i oa a
O O
•o <oCl gr
m jfco *CM 00m gr— o
• aO O
m mm gr
a£Q.3OacO
O
•o
a.3aacO
Xua.14V
ac rgpg
a1
— 4
OC l
eo
a^ i-4rg
00
Om^4O
o
* oPJ
c.
mv-4
Oe
O
a£ cr
C l
moO
o
ac co•-<CM
mooo
ae r»
Oa
o
•t J3—l
r j CM pgci sf in
g; ci pgcr - i c-o cr r-rg cp rg—4 O O
c ô c* - 4 ^ 4 ^ 4
ci vr in
co o CMcop- g;•C P - 0Drg co CM-< O o
O o ô
O O Oci gr m
r~ o tra> in cr— m r-—i o ci—1 ~4 O
a • aO O O
c^ cr crCM Ci J T
P- CM CD<r m gscr -4 cro o m-1 -H O
a a aOOO
oo co coPJ ci gr
CM C0 grr- CM cicr CM crcr ci gro — oa a a
o o or- r«- r»pj m gr
cr P- oo•O CM -4,4 -4 Oco • - ! mO -4 O
• • aOOO
<o « «i C M < n <»•
0 .
oceoo
f—
0 .
oacoX3d
u.
^ rO ffi mINJ f*> »t
,}• i r r-m -J" f>- - C <if1» ^ if>o ^- o
o c o
a pg pg pjPJ Cl ^
— cr O•JCJ - ^ C l
cr in o4- ci p-O -4 O
O O O
V -« -4 -CM c i gr
gr ci pg•»i œ -4-4 Cl O— * r-O >-4 O
O O O
* o o oPJ Cl gr
•o r- op- pg cr—i ce m•4 PJ COO ~4 O
a a aOOO
ac: cr cr cr•-4 pj rn
CM ci gro m g]P* C"" ClO CM Oo «g o
* a aOOO
JE co eo co-* I>J m
CQ CO CMO •"• **gr cr **
O --4 *-•• • •
min
m
CDf i
f\J
o
o
^in
0»t )rgPgU
O
ominp -
oC l
O
o
cr•4-
CMv-4CIClo
aO
CD
mCM
groa
o o o oK r- r- r
»-# rg pnr»gr
-'•ri-
r-or"~-O r> A,
o o o- O O
x r-r\j
O-mrtpo•-*
mO
r~tn
mCOO
of
o
r- r-
oCO
tr
or
-t - i o• o •
O O C
CC-ru
n"if \ j
c*
rr\
m,_,cc>oo
cr o:-t utr<G
o
: r- r- r-
— o o
CO
or^cr
«o
ccr\ j
CO
CO
!Zc
O
o
oo*
o
ccm
r j
CO
o«
o
r-r^m
C
o
tt" COJ If
IM
o
t
o
o
^1
en
e
oa
O
OJ-
i ra>r-r v i
C
ir~
c.a
C
c cIT ^cr
CD
r-C
•
o•Cf>,_(
a
c0
O
„
c
o**•o
o
cT_i r
I T
U'
c
c
r
x rv.
03
r».
c.
*
r\im
ir
^.oo
* a a c cr
•* tn —*
- O O• • *
O O O
— O C* m *
O O C
in cr CDJ3 O m
-i O -J—' . - O
^- 01 <VJr\j co r\jx O O
«^ O •-«m <"_ l/•O U' —— o o
• f to c o
<r oc co x
cr cr -ùr ^ * j - w*m CD ir»cr ~i - «
— o o« e p
O O O
fNJ C "-<a j 1 —CM O O
t • •
o a c
c e o•^ -* IT
1*1 C fjcr iri o.- o o• • »
o o o
o » ir
•o
oo
•om
i n
o
o
o
oo
« H O O• • •
o o o
ID h- m
—i — O* t •
o c o
-C ^ ""ri m i
o tr- r-tn»— oO T i ro en —«—< O O»«*
o o o
^ if. r*\-*> fv. —*- - O O
• • •
M O O• • •
c o o
f v J O O• • •
o c o
as
i/> ir in i
o-O**-
oO ' - ' O O
• * t> *
O O O O
ID -
• • • •
oooa© O O O«\i fl ^ .ï\
3OOfO
aaO
SCU
CD a.3O * O J O
O*-«OO a*• • • • O
aoooo
o*-<OO• • • •
OOOO
3
cc
0 0 0 0
QO —» O O• • • •
0 0 0 0
O O O O
00 -Û -4" rsicrooo
o*^oo• • • •
OOOO
c? a* 0" a-
a
O
a.O
a.
0 0 0
r * oto O O CD H O
• • • •0 0 0 0
OQf
fv
O O r O
o--*oo• • • t
O O O O
^ 0 0 0 0
a.Q
0 0 0
a j r r j.-« c- ote m r«
0 0 0
O N CD
O O O O
O
O
0
rg rr nj- » O O• • •
o o c
*t -T *r
• • •0 0 0
•0 « r~
O ^ HU
O O C
a.oor
n n ^• • •
o o o
It •* * •*
00 ^ r\i
cr r- -«
o — oft • ft
o o a
-100-
• * er•-t p~— co a
rr, rn r*'m .1 ir
13651
04556
re i"O O
e •O O
10396
04493
I\J S iTCC fn r*~ #H C Of*"1
^ O rO f*l 0* ™ ^ ^ V* •***co rv CO—- O^O * O / O
oc oo oo oo oo#0 f > 6 »• • B AS
oo oo oo oo oo
^t tJ"1* W^ kC **0 *<0 D ^ l * i * " *vi> QÛ 09 00 i^ O* Q* I
>û IT l*-iyp »$• If* r-CT" IT C*-4 CC •—f CD fNJ C M <£ <£ CT1 * ^pg ^r p*-r*" •>o o f^ ^ fNj ••*O* c* —i .-- c * - ' OO *0 Ooo ~*o oo ••* o oo
• • • • • • • • • t • •oo oo oo oo oo oo
ctf*\.—»
^3
•o
o
*
oo•
o
r(X)OfN
«o
r \ jU"o«
ro sT ^
CD 1*
-. oO tf-< a
w *
o o
m -*• tA
as r»
CD cr
^ o• o
o o
* -0 0 -Ûm ^ u*\
(r r-pn ,—.on "m *-*.— o
t •
o o
Vi r*" v^ro ••—> Oco in^ g^O C4 o
o o
OBCO
CO«t
o1—4
CO• *
p .
P J
oo
00i n
o o
[ *f *t <f 1^ i T i / \ I T ^ '<D ^ <C frt! !"*• •*** f***
0 .
o
ac
O
N GROUP .
FRCI
0.18989
0.05303
0.00619
* o o om -or in
,19099
,06092
,00904
a o o
x: cr (T cr
,21963
,05796
,01048
o o o
i t 00 CD 00CM CO 4"
o -e ao
oo CM in• * P - - 4
o o o
lit p- p- p-IM rO *
.27858
,06349
.01835
o a o
4<4)««I M r o *
0.05081
0.08813
0.02162
ÏÉ m m mIMPI +
ro gr pgCD ^ cr«mnin fj» roo o o
• a ,O O O
I t * • * *
D,
O
3O
CM
A GRCUP ;
urxu.
0.13965
0.06291
0.00538
rn •*• \f\
,16900
,05938
,00593
• • •o o o
* o o om >»• m
,17536
,06660
,00819
• w m
o o o
* cr cr crpg p^ - ^
,20621
,06152
,00905
v • •
o o oXt 00 00 00
IV 1*1 *
,24416
,07413
,01361
o a o
* p- p- p-rg ro *
0.28362
0.06230
0.01607
K « J3 <0CM rO *t
0.01785
0.C8416
0.02254
x: ir. i/i miv ro *
ro GROUP *
-0
4 GRCUP ;
FRCf
Û.12602
0.0512?
x: CM rw
,14586
,06135
o o
,14213
,05337
o o
X. O Oro *
15043
,06611
o o
pg m
,18209
,06182
• •o o
* 00 COCM CO
0.21781
0.07576
«; p» r-PJ pi
0.25811
0.06444
x: « gjpg co
rjm
,00491
O
-
MCJmooo
oin
,00697
O
cr
,00746
O
CO• * •
0.01155
0.01615
•o• * •
0 GROUP N
P»
r-
4 GROUP ;
4*L
oatu.
0.15535
0.03701
3& e*i m f*if« *^ <f\
,18659
o o
M; rg rg f\(m -gf i/\
f i CO r\jr m f\jf\j u*> ^r>i ir» Oru O O
O O O
t*\ %t m
12225
,05572
,00449
o o o
*: o o am •• in
,12939
,06732
,00599
o o o
x: o> o- »IM CO *
0.15661
0.06782
0.0C641
xt x ca coCM »O «4
gf cr coC*l »H Cp- - 4 sr0- Cf O
** o oo o o
Jt p- p- p-i\im«f
0 GROUP *
r~
00
a.gocO
Xucr.u.
<r iMin CM-< o
» «o o
rn **• in
ro *«
-i rCT r\J
.- oo o
x: 1*1 fo PIm ^ m
,23409
,032
51
o o
J£ IM IM PJro »* in
28346
04408
00311
o o o
ro 4- in
,09019
,04792
o o o
x: o a oro >* m
0.09546
0.06257
0.00442
CM CO s f
0.11555
0.06809
0.00473
a; oo uo coCM 1*1 •*•
0 GROUP K
I—
1 GROUP i
•B.
uu.
0.15341
0.00844
^ \f\ fcTt it'
,17440
,01416
o o
x: •» «c J*ro ^ incr cr(O -TCO p-
CM O
O Ô
^ Ifl r" rir o »v «TN
,27015
,02081
m m
o o
Xi IM IM INm * in
,33047
,03225
,00199
• • •O O O
X! ** »-4| r-4r o >••» m
0.05775
0.03917
0.02212
* o o oro •*• m
0,06113
0.05615
0.00283
i f cr tr crCM ro *
0 GROUP K
r"
O
1 GROUP 2
4K.
UCf.IL
ro ^m Oo corx Or- O
• t,
O O
SC -G -U -Oro <r tn
,16406
,00391
o o
x: in in mm <*• m
,18875
,00656
* *o o
x; -T •* •»ro -a in
2386B
,00810
o o
X! ro ro roro <t m
29775
,00964
o o
* CM r\J CMro •*• m
0.36688
0.02071
0.00092
ro *t m
0.02675
0.03033
0.00098
X O O Oro •» m
-101-
^ «• IT ^ C ^ J,** C O Q- -O «4 ru™ ^ OT (C h- .• *O O C O O O O
* « r o r f B
o o o o o o o
: Q G C. i»! ^^ t—» s£ f\j CM ^rr i r r . s; <* .tf^ u"* < *fr in • * ir* ^ ir <^ir
o o 0s f\j ry*<î O" *J Q- \f\•* -« O fSl *f*fr r- • - , - ( ©o o o o —• c •-* -« o <r
• • • • * • • i « Voo oo co o o c c-
cr o cr *: C c *: —< *-• *; r>j r\i :* r** r^ ^ ^ ^. a: ;/•« mm ,» tr •* in »* in ,yir ,j in ^ m , , ^
O r- m <j cr m ^••* rf"1 •* ^ j ri h- (y.
rw »H r n j cr OJ
inr i
ovCOCT*
i n•J*
f^i
r-ooo
ini n
D
O
Ï
04
9
IT-ir
co
jt g.
o
coc -. o « o ."-<c - _ o _p » • • « • «t • « , roc oc oo oc o o o o
'CDcrco n: o e tfco ^-^^-< ^rgr*. s^r^m ^gtgf- * i n i r•^gf 'n I^J? j*m g/ir gpm i j i r g^in g/m
- S S * S g? S S Sœc 1 o o r*- o cr irv —O O rj ,4j ^ ^. pry ^ ^«-* O ^ O «-«O ^-*C p-< O —• —< —«
• • • * « < • # " # • # » .
oo oo oo oo oo o o o
; r- t~- t~~ a: I L n, j t o t r st o t ai^^^-i M i oij a c r i f x *t *tfl iT IA r^»t r''. sj- ^-i/> *t \f\ -t it\ ^ m j-ii^
- " ' r ' O O n g ^ (^ ^ ^ m
C T ' N ^ « r ^ O - <f cr O .$• ^)f * > O O O r o u ^ O" iO o f>. pr—• ^ c c c r ^ - cr r- r- m j .•-< O r-JO - * O ^-*O i-«O - - O —i r-i
• • • • « • « * • * • • » • •oo ce co oo oc oc o o
: o « O ^ gtff-r- ' HÎODCD s ^ a c ^ O O ^ ; « - - iC(Nr«g *r"»ri
o Œ ^ t r <jh- ^, oc r». u*»»j f-C ^ O tC Of*- -4" 41 CO ^ « û (TO O r ^ O Q- -f —* OD CT1 O - * »T^ O «-I C i f > O ^- - - N- i f » O in*-• O »™«O M O i"jO r\iO —« O - ^ o •—'
oo oo oo oc oo oo oo o
*: -a o i SN *: cp co a f o c r ^ o o ^ ^ ^ ^ r-g (M
O co ^ o ^ ty* ^* CÛ ^ «T ^ r^•/) «T* f** ' ^ "O «O «^ O O «^ O ^JO»-» ^J-T O-O O O fvi h -fi-T^)»-i 0" —4 OO (%J PJ lT»O PJ i-ir-*O OO f<vO fsJO (MO —• O i-«O
oo oc oo oo oo oo oo oo
a d ^ - ^ - j stif\ifi K; -3 o3 s^r-^- ^ ao oo ^17-0* ^ o o ^^-*?^0 « IA 1 -^ ffl .j" f*t yf f*y if r ^ ifs »r »r*
O O Zf1 *t QD gf r-4«O O"^" CT Œ) »O 0s r*lt " O CC-sgt" »-4 CÛ IA D f^tO O f*» f\J OCCN^-t <o rsj cr>^> NO ^ h- ^ u"\m P-ogt O O CT sJ «l pij . 0 ^ ."^O ** O3t-4 f\j rtjINJO « - O — O OO <*>O IMO -^O -HO• • • • • • • • • • ft* • • • •
00 00 00 00 00 00 00 00
^ r*i m n X. ~t *t •* IA \T\ ^ <o o acr*-r^ ^ootn î^O1^ ^ 0 0ro ^ i ro *J ^^ f ^ *f ^^ r ^ ^^ 4~ i»o
^ ^: *: ^ «: *: ^ ^Cp-h* (g o co N aof*^ (j* tst r*-rn • ^"^ rg^>
et i-*rv ÛL K > o a t r \ - O û . r- * CL. o tf^ a- h - ^ j c i , 0 ^ 0 . J 1 ^3 ffc»-t 3 O O D ^ *O3 r*t m 3 f V 1 ^ ^ - O a D ^ O ï ^ - 3 u->OO » ^ O o u n r ^ o « û » ^ O e r r n o ^ f M O O O O c o ^ ^ o i r * ^et rt o a? M O n c *•* o ar r > O n t * o o n C r ^ o c t - ^ o ce - • oO • • O 9 * 0 • • O • • O • • O A I Ô • • LS • •
00 00 00 oa 00 00 00 00o a o o a a o ah- H> H *— M. »-. h- *—
^ (NI t\l r j s £ W ( ^ ^ * t - f i^U^iH ^ O " 0 MÏ^f^ ^ cO cO £ & 0"r^ ^ ^ ifl r^i ro ^ r*"( vf »^ r iA t*\ -f J3 fo * f** "n j CD f*^»^^ f*i rO ^1 wi f*i fi '•
cr ^ N- <ij Of*" r*f*- •j'Cr aocr r*« - ^^">Ja O N <L h - r ^ - a c o i ^ a . c e m c u «4 - - Q, m <o a. c r o o . «•-«3 rarsi 3 s f c o ^ m ( ^ 3 « > r f > 3 o o e r o u o ^ - 3 m o ^ ^-rO C ? 1 ^ O H M O 0 > O L J O "û O > f f * " l O O f ^ o i n ^ C J ^^^a^et m o o a m a c e p g o o e ^ O a c o O n £ o o at « M O Q C —OO • • • O • • O • • O • « O » • O • • O • • ij) • «
0 0 0 00 00 oa 00 00 00 00X X X f X X Z Xo a a o a o o oac x-*-*-* ot v: N N a. ii<i«i ce x-i--*- a ^u\m a * -o <o QL ^ p- r- QC M: auu, f l >/ tA y. 'H u. r ^ - X i i » f O - ^ i t ci *f" IL, r n ^ f u . ^ « t u . **\ *j
-102-
X
3D3o
•m
3Oae
JJOetl i t
aooo
x oo ot.» m
m
mr»
O
X f- f»«t m
ôX -0 -O
.» iro>PJmMp <
•O
X tn ir><» m
m .mm•
o
X •* ** m03
•ûtnm*
Ô
X m m* mN
00m -P 4
O
X CM ex•*• mCM O•4 OO (M0» CMO OO Ô
X • * • *« m** m
0< mo o• to o
X O O<* m
•4 a»p* (M- 4 «O*4 O
O O
xo» o»
xa.§aeo
o
o•r
a.3aae«0
o
u.
CM
00
o•
o
X 9 0>^ &momO
O
X co a)* m
mm
O
X f- 1* m
p 4
m
ôX * «
•r m<M0P
om
Ô
x m m* m• *
•o
•o
X * • *
»a i
om
o
x m m* mCMp 4
CMm
o
X N CMs» m
O Q>•4 m
m Mes o• •o o
X "4 "4«fin• ^ CMoo m•«r *
m *O O
o ox oo
«r m
xa.8So
a.3Oaeo
RC
M
u.
mCD*fC
r
O
X O Cm «o
tn00
oo
x v crt# m
« 4
•1-« 4
• 4
O
X 00 OD^ IT
«t
Ô
x f- r~-*• m
mas
- 4
o
X 4] «0.» m
ro
ôx m m
«t tn
<ntn•ù—<
o
X • * • *«r m
mI MP 4
•ft-t
O
*f m(M03
(2.•4
1O
X «x CM
•t m00 10
CM U>CM (M
o o• •
o o
X ****•* i n
xa.oaeu
a
CM
3Oato
ROM
t ^
mcea-rvO
eO
X »-in
ocf»"
co
X Om•bmm00
oô
x a•*ro•am, •4P 4
O
X CO
o(M00
p 4
C
x r»«t
oo00mP 4
O
X «
osIM
•O
x m
m
o
x •*
«I-
ÔX "1
00MODp 4
P 4
O
X CM• »
X
a.Oaeo
o
try
a.3aœo
uaeu.
X (Mt r
r«-a<cif
oo
X —mCM
mtr
oo
X Ot r
»
mO
Ô
x a
•oo• M
m
O
X 00
oor-
o
X r>-«t
OD
«0
a
x «•*f .fw«0IMP 4
O
X tr
o>«M
m
t
o
X «•*
p *
lf\m
4O
X Cl• *
X
û.
o
3a
«r(X3Oae19
Uet
x cim
X (Mi n
#»*• 0
mr**oo
X ««in<•*•a00a>O
X Om• •o0 s
CM
X »"*mm
O
x ou•*i »<D
m**
ô
•t0>mtnCM
O
a «•rr*
m•o
O
X m
• •
o4fft
O
X *
X
a3
ace«9
o
m•r
&3aaeoaxu.
X «tn
X dm
X CM
mOOmOota
X xmomF*-
o•
X Omof -
ooo
X V«t
ot -f -<p
oô
X <S
oOOmO
ôX f-
«roCM• 4vOO
o
X O
o«0moo
x m*
xa.oae
o
4»>
Ou3oaeoaaea.
x mm
X *m
x mm
X CMmommr-o
ôX ->
mooo
o
X OmO
CM
Ô
X »
o<«>mo*oo
X 00
oo> • <
o
x r-
o
moo
• > -i•r
-103-
OIP
O
* •» * ITIT
oOS
oo
: oIT.
oIS
00
o
4n
O
oo
3oofooPh.
• * •
0.
osXoat
OOO<ooo
x at&
oasIM
oQ
X P"
a.3Ot±
o
a.3aaoXaat
om•ooo
oa-i / \
oo
K OD
a3OorO
o
a.3a6Xoacu.
o*01 0• f
oo
« oIT
ointni ^
O
O
*
a.3c
Q
Oi n
a3aaoaata.
o
oo
M - •mOirCE
o•o
a om
Q .
3OaruQ
mA.
Oac
oaa.
m
o•o
ABSORPTION
K1
1121314151
00,00,00,
.0
.0
.0
.0
.0
.0
CROSS
K212223242
00Q00
SECTIONS
.0
.0
.0
.0
.0
K313233343
FOR
00,0,0,0,
ZIRCONIUM
.0
.0
.0
.0
.0
K414243444
ELASTIC SCATTERING CROSS SECTIONS FOR i
K1112131415X
0,1.2,5.6.7.
.38400,06800,78400.71975,96325,46550
' K212223242
0,1,3,5,7.
.42075
.18575
.01275,98500,78800
K313233343
INELASTIC SCATTERING CROSS
K1U21314151
1.1.a.0.0.0.
73000590C049000000
K212223242
1.1.0.0.0.
,7300054000,4200000
AVERAGE GAMHA ENERGY IN
K1U21314151
8.3.0.0.0.0.
649990000098C00000
K212223242
7.2.0.0.0.
85000700009700000
K3
13233343
0.1.3.6.7.
.49400,27400,19125,13350,47600
SECTIONS
1.1.0.0.0.
7200049000340000.0
K414243444
FOR
K414243444
INELASTIC COLLIS
K313233343
7.2.0.0.0.
00000400009600000
K.4
14243444
000,0,0,
.0
.0
.0
.0
.0
K515253545
EIRCONIUM
0,1.3,6.7,
,55900,42800,45100,42 400,16000
K515253545
ZIRCONIUM
1.1.0.0.0.
71000,43000,2700000
ION WITH
6.2.0.0.0.
40000C500095CJ00
c
K515253545
L
K515253545
0,0,0,0,0,
0,1.3,6.6,
1.1.0.0.0.
.0
.0
.0
.0
.0
.63 750,57500,65800,64400,75000
70000,34000,220000,0
IPCONIUM
5.1.0.0.0.
70000650009400000
K616263646
K.6
16263646
K616263646
K6162'-.3646
0.00.00.00.00.0
0.681501.755003.905256.858757.09800
1.69000l.??0000.150000.00.0
5.100001.30000C.930000.00.0
K717273747
K.7
1 7273747
K7
17273747
K717273747
0.00.00.00.00.0
0.715001.925004.347006.966008.4160Q
i.69C001.020000.06COO0.00.0
4.650001.150000.930000.00,0
K
s18283848
K813283848
K818283848
K.818293a48
0.0.0.0.0.
0.2.4.6.7.
1.0.0.0,0.
4.1.0.0.0.
000
c0
7010018400699008062586250
68C0O80000000
20000
orooo000
K9
19293949
K9
19293949
K9
19293949
K919293949
0.00.00.00.0
n.o
0.877502.422505.063256. 720007.386'JO
1.65000fi.660000.00.00.0
3.800001.020000.00.00.0
K1020304050
K1020304050
K1020304050
K1020304050
0.00.00.00.00.0
•
0*954 502.616255.453006.754507.05000
1.620000.560000.00,00.0
3.400001.000000.00.00.0
1
1ï
SCURCEIt5,9,
13,17,21,25,29,33,37,41 ,45,49,
SPECTRUM1.000004.8644415.7241429.8245136.7803339.3127131.6483323.6267116. 6172012.401926.972093.679372.64709
2,6,10,14,18,22,26,30,34,38,42.46,50,
1.063226.7597021.4433435.8758740.8655541.8116632.4532023.6826614.766009.074995.414293.560162.03625
3,7,
lit15,19,23,27,31,35,39,43,*7 ,51,
1.834019.4393321.7974535.2019845. 1665036.6891629.777852J.2566414.526698.847965.253353. 430941.95912
4,8,
12,16,20,24,28,32,36,40,44,48,
2.8555812.5097431.8654340.6275836.7880438.2656426.8105218.45610li.090617.175535.C75972.75243
oVJ1
MATERIALS IN THE REACTOR
MATERIAL
ALUMINUMCARBONOEUTERIUMHYDROGENI PONGXYGENURANIUM 235URANIUM 238Z 1RC0NIUM
REF. NO.(MPRi
1210g91311Z614
MASS<AMU>
26.733911.90801.99560.998555.336115.8526
232.9021235.882190.3862
ALPHA
0.860V70.714120.110460.000000.930260.7767?0.982970.983190*95671
CSI
0.072980.158920.726430.999990.035710.121020.008560.008450.02197
TRANSPORT CORRECTION APPLIED TO WRl GEOMETRY
GECHETRY DEPENDENT INPUT DATA
FIM1 1
0 . 0
o.c
0 . 0
0 .0
0 .0
0.3660
0.6390
R( I)
0.1500
0.4000
0.6338
0.7611
0.8836
1.2646
1.6456
J
234567B9
THE
THE
1
12
123u56
123456
119
108
213
306
SAKE AS
SAME AS
910
9101411
23C6
910
i l3
ÎOfc
i\ N( l , . ' lU0**24AT0HS/CCI
10.0000527000.0000000010.OC00000010.0000000010.0000000010.OOOOOOQOl0.0000000010.000000001O.OOuOOOOOl
REGION 1
REGION 1
0.043030024
0.0316991810.Q409Z1271
0.0099288600.0128lfcfl5B0.0CB350OOO0.0225200060.0002600000.0109H999B
0.0028879790.0037?81360.0040099960.037630022C.0004400000.018369973
OO5I
-107-
U~> - O 0s (J1 O 31
O IT iT ^ O' ^
J? f" fi pf> O "OO O O n"* O —*o o o o o o
o o o o o o
^ N J ifCE (J- 0 —•
"^ %r o o o i"w r- O f~ O CTO- .C O O" C 1 T- < o o CT- o : r
CO
^ M O -- OOo o o o o o
o o o c o ooo
o o o*H i - 1 Û N û Ûa o o a o o
o o ^ o o o
r j C O cr a o
^ T O O O O
rg r<i m r- O tfO O O m O —o o o o o ou o o o o o
•y & o o o —•y"> * r o o c • o—< Xi o O C OCJ C f"\j (T ^-t r\j
C O O r*i C —'O O O O O O
O O O û O O
4 CT1
•T C
£ a
i-i O
c»oa*T
o
O
o oo oo o) _
•C Oj—« O
o o
(7
1tnoo
o 4- — «y of— -« — O
-oo
o
15
16
17
18
19
20
21
22
23
24
25
26
0,
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
0.
.c
,0
,0
0
,0
c
0
c
0
0
0
0
4.1603
4.2644
4.8500
5.5000
6.0376
6.1900
7.0000
8. 0000
9.0000
IC.0000
11.0000
12.3 359
THE
1
12
THE
THE
1
123
THE
THE
THE
THE
THE
SAME AS
13
1011
SAKE AS
SANE AS
12
Bil9
SAME A5
SAME AS
SAME AS
SAME AS
SAME AS
REGION 5
0-086269975
0.000026000O.OCOO52OOO
RÉGION 17
REGION 17
0.060500026
0.0663999920.0332999830.000070000
REGION 21
REGION 21
REGION 21
REGION 21
REGION 21
O00
THE FOLLOWING DATA IS NORMALIZED TO O.IOOOOGOE 01 KWttTTSOF U235 F I S S I O N ENERGY PRODUCED PER CM THICKNESS OF LATT ICt CfLL
INTEGRATED FLUX ( N / C M » * 2 - S E C I AS A FUNCTION OF RADIUS
FLUX
0.1246307E 140.1246308E 140.1246308E 140.1245873E 140.1236958E 140.1265656E 140.1273732E 140.1233661E 140.11ST872E 140.1144204E 140.1125383E 140.UO8879E 140.1033788E 140.8983080F. 130.7861962E 13O.77560B8E 130.6913822E 130.6476210E 130.6201104E 13C.6222144E 130.5329843E 13O.43818I4E 130.3659159E 130.3162385E 130.2B454t3E 13O.2649338E 13
VOLUME WEIGHTEDAVERAGE RADIUS
(CM)
0.100000.293940.525710.69939O.823B71=085361.463411.842682.222552.412592.612732.993143.373683.754324.C51924.21259'..5o3465 . 1 8 1 8 05.772976 . 1 1 4 1 16.603287.51UO8.509799.5087610.5079211.DB067
oCDI
-llO-
ooc
a
o3
4
LUZLU
Z
1 52 2& z
LU
3LU
I(M UJ UJ tu IU UJ UJ UJ UJ \U UJ U IU LU MJ IU IM Mi U Ul UJ LU iU UJ LU UJ IU UJ UJ ' ' UJ UJ UJ IU UJ liJ UJ UJ
v m 4 ) O Q o ^ 4 r M f t # r « > i r * ? 0 > r \ r « D O O O ' ' > r o b ( r 3 > < \ j e * i f < > > r r '
o3 3 • "
U, O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O
FLU* CM/CH*»2-SEC> PER UNIT ENERGY AS A FUNCTION OF ENERGY IN REGION
FLUX ENERGY ESAR IN MEV
C.10J4821É0.1769291E0.2979540EC.5095376E0.8488754E0.1274036EO.188O7OOE0.2607234E0.3575237EO.*587O73E0.5686042E0.7216339E0.101?829E0.1251119E0.14357C6E0.1618992E0.1753372E0.1905554E0.21275T3E0.23527l9BE0.2768914E0.S049904E0.3319219E0.3750687E0.3905515E0.432468BE0.5420863E0.594S460E0.5937227E0.649882CE0.6604735E0.6931127E0.6828309E0.5778707E0.5176332EC.8123063E0.9456791E0.9742685E0.1O1273OE0.1027562E0.1071947E0.1114445E0.1161501E0.1212065E0.1240763E0»12829gCE0.13663PIE0.1433152E0.1^9C939E0.155C793E
1111111111121212121212121313131313l-i13131313131313131313131313131313131313131414141414I t1414141 *1 *I *
9.542978.693927.944897.244386.595486.020845.496235.021654.571324.172573.796513.447833.147632.873192.623032.398632.198491.998341.823991.673891.523771.386561.261431.149281.U49210.954300.869390.794490.724440.659550.602080.5496 20,502160.457130.417260.379650.344780.314760.287320.262300.2 39360.2198 50.199830.IB2400.167390.152380.13B660.126150.114930.10492
FLUX IN/CM»*2-i£.r I PER UNIT ENERGY AS A FUNCTION (IF EN^HG* RtGION 13
FLUX AT
O.3957235Ç 100.1526650E I I0.2577801E 110.4395161E I I0.7312546E 11C.1CÎ7207E 120.16156I8E 120.221890TE 12Q.3040762E 12C.3901834E 1Z0.4800334E 120.6O34550E 120.8437453E 120.1052939E 130.1202659E 130.1361392E 130.14716316 130.1602047E 130.1786440E 130.1962862E 130.2298330E 13C.2500216E 130.266'»7fclE 130.2945151E 130.3071475E 130.3381<.68E 130.4286405E 130.4716776E 13O.*7^.53È5E 130.5141799E 130.522B744E 13
0.5449476E 13G.4530466E 130.4087727E 130c6<.535«lE 13Û.753757SE 130.775992'iE 130.8098102E 130.8317954E 130.8682<^8<iE 130.9077968E 13C.<5'i9610aE 13O.1O11558E 1 *0.1031533E 140.1076697E 140 t11663C6E 14C . 1 2 J 7 9 0 3 F 140.1290658E 14
ENERGY EBAR IN HEV
9.54297B. 693927.944897.244386.595486.020845.496235.021654.571324.172573.796513.447833.147632.873192.623032.39P632.198491.998341.8 23991.673891.523771.386561.2 614 31.149281.049210.954300.869390.794490.724440.659550.6020S0.549620.502160.457130.417260.379650.344780.314760.287320.262300.239B60.219650.199830.182400.16739O.lb23a0.1336b0.126150.11493rv. l n4<>?
tv.i
HLUX (N/CM»*2-SECI PER UNIT ENERGY Ai A FUNCTION V.f ENfRGV IN REGION 24
FLUX
0.2055851E0.3542197E0.6037971E0.1030565EO.1757100E0.2551260E0.3723633E0.4711875E0.6367606E0.7767477E0.6357957EC.9753959E0.167598CE0.2375443E0.2632347EC.3033067EC.31224C4E0.330572eE0.370378fct0.3974193E0.5024224E0.S540178E0.56i4356EC.6304597E0.625B799E0.7125663EC.1085453E0.1273497E0.1359867E0.1479390E0.1580709E0.174307BEO.18C39*3E0.1434901EC.124O158E0.2275090E0.2880671E0.3lb4 74lEO.3457664E0.3 76002 9EL.409 Id2 8E0.44693'JIEC•492 30 f 4EC.544O2C 3EC.5876 04 4E0.64173É6E0.712087OEC . 7B54 398fcC« 6o01943E0.9381JSOE
A T
1010101 1111111U1111111112121212121212121212121212121313131313U13131313131313131 Î1 3131 31 313l i1 11 31 i
ENERGY EBAR I N MEV
9.542978.693927.944897.2443 36.595486.020845.496235.021b54.571324.172573.796513.447833.147632.B73192.6230^2.398632.198491.998341.B23991.673891.523771.386561.261431.149231.049210.954300.869390.794490.72444O.t59550.602080.549620.502160.45713Û.417260.3T9650.344780.314760.28732C.2623D0.239860.219850.199830.18240C.167390 . 1 5 2 3 80.I3B660.126150.114930.10492
-114-
ooata
CD
O
O
Oetazai
OCUJ
uz
Oce
• z• UJ
1JJ UJ I U MJ I U l i J UJ M l I I I i l l l u t i l m I I I I I I l i t t i i i l l m i l l I I I I I I i n n l H i m l l i t , f 111 i . l H I i | f t i l i l t I t l H I ^f n i i l f i l l I I I m 111 111 I I I H I t i l I I I I I I I I I
UJ 3 QD^4rMirtiO<riiHi
4 u. O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O O Cl O O O O O O O O O O O O
AVERAGE FlUX IN/CH*»2-SEC) PER UNIT ENERGY, WEIGHTED BV CARBON
FLUX AT ENERGV EBAR IN MEV
0.8228467E0.1406507E0.2364926E0.4042881E0.6745962E0.1009119E0.148807060.205489<>E0.2811614E0.3593288E0.4427138E0.5593988E0.7876793E0.9762594E0.1124849E0.1272994E0.13781U4E0.1500122E0.1677494E0.1B49553E0.2168790E0.2367956E0.Ï548167E0.283b2<>3E0.2963771E0.3268065EO.*U9*15E0.45«53l*FO.«5a*262EC.V983706E0.5082090E0.S336936E0.5327764EQ.*5*012*E0.*0<52265E0.6326-VL1E0.7378231E0.76253C3E0.7998031E0.8212216E0.8598381E0.9012KJE0.9't<ilb&<sE0,1006137EO.IO2T937E0. 10f«,l6 3EO.ll'>'.Të?E0.1Z-.575eEO.lZ'ÎOTl^E0. U^OIO'-E
10111111111212121212121212121313131313131313131J13
9.5^297B.693927.944897.24433b.59548S.020845.496235.02165i.S7132i, 1725 7i. 79651J.44783Î.147632.673192.62303Î.398632.19849L.99B341.823991.673891.52377•3E656
L.,26148L.149281. 04921
13 0.9H3013 0.8693*13 *(13 (
3.794493.72444
13 0.6595513 0.60208l i (13 [13 (
).549623.502163.45713
13 C.1T2613 0.3796513 0.3M.JB13 t3.3147613 0.2873211 0.26230l i 0.23986H C.2198513 0.199831". C/ . 1824.-014 C.167391<. 0.152381 4 C1 " . C
^.13966\ 12615
1*. 0.114931 4 Ci. 10492
THE FOLLGWING DATA IS NORMALIZED TO O.1O00000E 01 KWATÎSOF U235 FISSION ENERGY PRODUCED PER CM THICKNESS OF LATTICE CELL
TOTAL KINETIC ENERGY TRANSFERED = 0.2038846E 02 WATTS
ENERGY LEAVING CELL THROUGH CELL BOUNDARIES = 0.BB417B9E Oi WATTS
ENERGY ENTERING CELL THROUGH CELL BOUNDARIES = 0,884178^ 01 WATTS
TOTAL ENERGY LOST THROUGH CELL BOUNDAklES = 0.0 WATTS
TOTAL ENERGY LOST THROUGH LOWER ENERGY BOUND = 0.7559372E 00 WATTS
TOTAL ENERGY INPUT » 0.2521394E 02 WATTS £
TOTAL FINAL ENERGY = 0.2525114E 02 WATTS
OF WHICH 0.3044981E 01 WATTS COME FROM GAMMA RAY ENERGIES IN INELASTIC
SCATTERING COLLISIONS, AND 0.1061797E 01 WATTS COME FROM NUN-CENTER-OF-M&SS
ENERGY IN ABSORPTION REACTIONS
KINETIC EKERGY TRANSFERRED IN REGION 1
MATERIAL
OXYGENHVOROGENCARBONDEUTERIUMALUMINUMZIRCONIUMURANIUM 235IRONURANIUM 238
ENERGY TRANSFERREDIMATTS/GRAM)
0.2443530E-010.2554TUE Cl0.3954T54E-010.8B24A70E 000. 8256<H9E-020 . 125Ù762E-020.2157812E-030.2073074E-020. 225<H05E-03
ENERGY TRANSFERREDIHATS)
C.2395783E-O50.2993701E-090.5526B37E-100.2066715E-090.2590600F-I00.1333156E-100.5898010E-HC. 13'.62<59E-10O.6253886F.-11
KINETIC ENFRGY TRANSFERRED IN REGION 6
MATERIAL
HYDROGENCARBONZIRCONIUMOXYGENURANIUP 23SURANIUM 238
ENERGY TRANSFERRED(WATTS/GRAM)
0.2600850E 010.4030866E-010. 1280183E-02
O.22OO38OE-O3
ENERGY TRANSFERRED(MATS)
C.1100775E 000.262A364F-01
0.37882B9E-010.5668268E-0*0.25*8683F-02
HINETIC ENERGY TRANSFERRED IN REGION 13
MATERIAl
HYDROGENCARBGNZIRCCNIUMCXYGENURANIUM 23 5
238
ENERGY TRANSFERRED(WATTS/GRAM)
0.2136198E 010.3322593E-010.1052377E-02O.2035O21E-010. IB1959"'E-O30. 1901B92E-03
ENERGY TPANSFfcRRfD(WATS1
O.13«32T1F 00O.3215O5OE-O10.4739699E-02o.isî ' .giaE ooO.23273T«.F-O3O.IO3<>7BOE-O1
KINETIC ENERGY TRANSFERRED IN REGION 24
MATERIAL ENERGY TRANSFERRED ENERGY TRANSFERREDtWATTS/GKAM) (WATS)
DEUTERIUM 0.1754680E 00 0.2304249E 01OXYGEN 0.49414936-02 0.258519LE 00HYDROGEN 0.5527105E 00 0.3828544E-02
0.2131985E Cl WATTS WERE TRANSFERRED TO HYDROGEN
0.5025066E 00 WATTS WERE TRANSFERRED TO CARBON
0.1G92623E-C2 WATTS WERE TRANSFERRED TO URANIUM 235
0.4835545E-01 WATTS WERE TRANSFERRED TO URANIUM 236
THE TOTAL KINETIC ENERGY TRANSFERRED BETWEEN REGIONS 17 AND 26 IS 0.1694189E 02 WATTS
ooi
THE FOLLOWING OATA IS NORMALIZED TO O.IOOOOOOE 01 KHATTSOF U235 FISSION ENERGY PRODUCED PER CM THICKNESS OF LATTICE CELL
NICKEL FOIL TES? CASE
THE CROSS SECTION DATA IS AS FOLLOWS
L*8*IS,22?29,36,43,50,
0.660000.590000.200000.013500.00.00.00.0
2,9,16,23,30,37,44,51,
0.665000.560000.1*8000.008700.00.00.00.0
3,10,17.2*,31»38,45,
0.670000.510000.103000.006100.00.00.0
11,IB,25,32,39,46,
0.675000.435000.071000.003600.00.00.0
5,12,19,26,33,40,47,
0.65000O.35OOO0.046000.001500.00.00.0
6,13,20,27,34,41,48,
0.62500O.290000.029000.001000.00.00.0
7,14,21,28,35,42,49,
0.610000.247000.020000.00.00.00.0
0.3865601E 02 DISINTEGRATIONS PER SECOND PER MG. PER MINUTE OF IRRADIATION IN REGION 1
EFFECTIVE FLUX = 0.9097799E 13 N/CM«*2-SEC
0.3964046E 02 OIS INTEGRAT IONS PER SECOND PER MG» PER MINUTE OF IRRADIATION IN REGION 6
EFFECTIVE FLUX = 0.9329492E 13 N/CM**2-SEC
O.3355O7OE 02 DISINTEGRATIONS PER StCOND PER MG. PER MINUTE OF IRRADIATION IN REGION 13
EFFECTIVE FLUX = 0.7P96253E 13 N/CM«»2-SEC
0.5690973? 01 DISINTEGRATIONS PER SECOND PER MG. PER MINUTE OF IRRADIATION IN REGION 26
EFFECTIVE FLUX = 0.13393B6E 13 N/CM**2-SEC
THE FOLLOWING OATA IS NORMALIZED TO O.1000000E 01 KWATTSOF U235 FISSION ENERGY' PRODUCEO PER CM THICKNESS OF LATTICE CELL
IRON FOIL TEST CASE-FE54IN,P)HN54
THE CROSS SECTION DATA IS AS FOLLOWS
1,8,
15,22,29,36,«3,50,
0.640000.536000.131000.013000.00.00.00.0
2,9,16,23,30,37,44,51,
0.655000.488000.09Z000.008800.00.00.00.0
3,10,17,24,31,38,45,
0.657000.406000.073500.005400.00.00.0
4,11,18,25,32,39,46,
0.645000.334000.062400.003200.00.00.0
5,12,19,26,33,40,47,
0.626000.285000.048700.00150G.O0.00.0
6,13.?0,?7,34,
41 ,48,
0.598000.22*000.033000.00.00.00.0
7,14,?1 ,28,35,42,49,
C.580000.174000.021000.00.00.00.0
0.6*17570E 00 DISINTEGRATIONS PER SECOND PER MG. PER MINUTE OF IRRADIATION IN REGION 1
EFFECTIVE FLUX = 0.1111776E 14 N/CM**2-SEC
0.6581255E 00 DISINTEGRATIONS PER SECOND PER MG. PER MINUTE OF IRRADIAI ION IN REGION 6
EFFECTIVE FLUX = O.114O133E 14 N/CM*«2-SEC
O.55755OOE 00 DISINTEGRATIONS PER SECOND PER MG. PER MINUTE OF IRRADIATION IN REGION 13
EFFECTIVE FLUX = 0.9658961E 13 N/CM**2-SEC
0.9508288E-01 DISINTEGRATIONS PER SECOND PER MG. PER MINUTE OF IRRADIATION IN REGION 26
EFFECTIVE FLUX « 0.1647211E 13 N/CM**2-SEC
O
Additional copies of'this documentmay be obtained from
Scientific Document Distribution OfficeAtomjc Energy of Canada Limited
CrTalk River, Ontario, Canada
Price . $2 .50 per copy
'622-70