diffraction effects on ultrasonic waves
DESCRIPTION
by Karim Jezzine and Alain Lhémery French Atomic Energy Commission CEA - Saclay. Diffraction Effects on Ultrasonic Waves Radiated by a Transducer Mounted on the Section of a Guide of Arbitrary Geometry. Context of development Theory brief review - PowerPoint PPT PresentationTRANSCRIPT
Diffraction Effects on Ultrasonic WavesDiffraction Effects on Ultrasonic Waves
Radiated by a Transducer Mounted on the Radiated by a Transducer Mounted on the
Section of a Guide of Arbitrary GeometrySection of a Guide of Arbitrary Geometry
byby Karim JezzineKarim Jezzine and and Alain LhémeryAlain Lhémery
French Atomic Energy CommissionCEA - Saclay
• Context of developmentContext of development
• TheoryTheory• brief reviewbrief review• adaptation of Semi-Analytic F.E. methodadaptation of Semi-Analytic F.E. method
• Validation in the axisymmetric caseValidation in the axisymmetric case
• Transducer diffraction effectsTransducer diffraction effects• influence influence of aof apertureperture // bandwith bandwith in the in the a axisymmetric casexisymmetric case• 2D case2D case: : rectangular cross sectionrectangular cross section
• Summary – Summary – WWorkork in progress in progress
Context of developmentContext of development• industrial needs for simulation tools dealing with guided waves in CIVA (software platform for NDE simulation developed at CEA)
- prediction of transducer diffraction effects to optimise testing configuration (mode selection etc.)
- simulation of radiation, propagation, scattering by a defect and reception• aims: guides of arbitrary section
computer efficiency => 3D computational methods hopeless• 1st application: unusual configuration of testing where the transducer (emitter/receiver) is mounted on the guide section
z
transducer
waveguide
guide axis
S
guide section
• Context of developmentContext of development
• TheoryTheory• brief reviewbrief review• adaptation of Semi-Analytic F.E. methodadaptation of Semi-Analytic F.E. method
• Validation in the axisymmetric caseValidation in the axisymmetric case
• Transducer diffraction effectsTransducer diffraction effects• influence influence of aof apertureperture // bandwith bandwith in the in the a axisymmetric casexisymmetric case• 2D case2D case: : rectangular cross sectionrectangular cross section
• Summary – Summary – WWorkork in progress in progress
Theory: Theory: brief reviewbrief review
• basic idea: benefit of the symmetry of translation to restrict computations to the guide section modal decomposition
n nnn
n nnn
tzkj
tzkj
n
n
eyxAzyxAzyx
eyxAzyxAzyx
)(
)(
),(~),,(),,(
),(~),,(),,(
nn
nn
σσσ
uuu propagation along z
mixed: either ux, uy,zz , or, xz,yz,uz at z=0
pure: either ux,uy,uz , or xz,yz,zz (e.g.: piezo transducer in direct contact) at z=0
modal decomposition : un , n
imposed end conditions: mixed or pure• find An knowing :
• direct projection of the source terms on the mode basis impossible for pure end conditions
nzz(n)n(source)zz
nyz(n)n
nxz(n)n
σAσ
σAσA
~
~0~0
minimisation of residual boundary values at z = 0
Gregory & Gladwell , Quart. J. Mech. Appl. Math. (1989) Puckett & Peterson, Ultrasonics (2005)
• requirement: initial computation of modes
- roots of analytical solutions (dispersion equation) for multi-layered plates or cylinders (expl. Disperse, NDT group at Imperial College)
Lowe, I.E.E.E. Trans. UFFC (1995);
+ : « exact » dispersion equations – multi-layered- : two geometries only (plate, cylinder)
- Semi-Analytical Finite Element (S.A.F.E.) method:
Dong & Nelson, J. Appl. Mech. (1972); Gavrić, J. Sound. Vib. (1995); Hayashi & Rose, Mat. Eval. (2003);Damljanović & Weaver, J. Acoust. Soc. Am. (2004);
+ : arbitrary section + easy to account for anisotropy, viscoelasticity
- : computer intensive at high frequencies
Theory: Theory: brief review brief review (contd.)(contd.)
computation of modesin complex cases
Theory: Theory: adaptation of SAFE to pb. of radiation from the sectionadaptation of SAFE to pb. of radiation from the section
• meshing of the section by finite elements:
elements: 1D (plate/axisym.) 2D (arbitrary section)
0)( 22 iiii3
i2
i1 dMdKKK kjk
• application of the principle of virtual work at the i-th element:quadratic eigensystem (size 9x9) in k
)(),(])[;,,,( tkzji eyxikzyx dNu
matrix of interpolation (quadratic) functions
nodal displacement
z-propagator
• displacement field at the i-th element (for 2D case):
Theory: Theory: adaptation of SAFE… adaptation of SAFE… (contd.)(contd.)
• assembly of a 3M x 3M quadratic eigensystem (M nodes)
0)( 22 MddKKK 321 kjk
• once solved: 6M eigenvalues (wavenumbers)
- real values: propagative modes- imaginary values: evanescent ‘’- complex values: inhomogeneous ‘’
6M eigenvectors (corresponding displacement)
1st elt.
2nd elt.
(system #1)
• account of source terms in SAFE:
- existing: on the guiding surface source modelled as an external force
Liu & Achenbach, J. Appl. Mech. (1995), Zhuang et al., J. Appl. Mech. (1999),Hayashi et al., J. Acoust. Soc. Am. (2003)
- here: on the section
problem closely related to that of the scattering from the free end of a semi-infinite guide:
SAFE: - Rattanawangcharoen et al., J. Appl. Mech. (1994), - Taweel et al., Int. J. Solids Struct. (2000), - Galan & Abascal, Int. J. Numer. Meth. Engng. (2002)
Le Clézio, PhD thesis Bordeaux 1 University (2001)
=> source modelled as a vertical boundary condition
Theory: Theory: adaptation of SAFE… adaptation of SAFE… (contd.)(contd.)
Theory: Theory: adaptation of SAFE… adaptation of SAFE… (contd.)(contd.)
• source mounted on the guide section at z = 0:
- one selects modes (obtained from System #1) that make sense for z > 0: 3M - stress tensor deduced from eigenvector displacement at the M nodes (xi , yi )
- piston-source modelled as source of normal stress
M
niiyz(n)n
M
niixz(n)n
M
niizz(n)nii(source)zz
yxσAyxσA
yxσAyxσ
3
1
3
1
3
1
),(~0),(~0
),(~)0,,(i = 1,…, M (system #2)
• time-domain solutions obtained by Fourier synthesisin system#1, the various matrices are frequency-independent, not the overall system
• Context of developmentContext of development
• TheoryTheory• brief reviewbrief review• adaptation of Semi-Analytic F.E. methodadaptation of Semi-Analytic F.E. method
• Validation in the axisymmetric caseValidation in the axisymmetric case
• Transducer diffraction effectsTransducer diffraction effects• influence influence of aof apertureperture // bandwith bandwith in the in the a axisymmetric casexisymmetric case• 2D case2D case: : rectangular cross sectionrectangular cross section
• Summary – Summary – WWorkork in progress in progress
Validation in the axisymmetric caseValidation in the axisymmetric case
d
transducer E cylindrical guide transducer R
receiver output
2/
0),()(
d
z drrtrvtO
• Simulation of a transducer in reception
d
• (System #1) + (System #2) + IFFT:
d
transducer cylindrical guide
zfield points
field prediction
Validation in the axisymmetric caseValidation in the axisymmetric case
2/
0),(
)(d
z drrtrv
tO
• (very recent) example from Puckett & Peterson (Ultrasonics 43(3), 2005)
configuration:- d = 25 mm- z = 250 mm- fused quartz- piston-like transd.- Gaussian pulses: 1107 kHz – 6.7 % of relative bandwidth
(12 prop. modes)
d
transducer E cylindrical guide
z
transducer R
measured (Ultrasonics 43(3), 2005)60 80 100 120 14040
simulated (present model)60 80 100 120 14040
• Context of developmentContext of development
• TheoryTheory• brief reviewbrief review• adaptation of Semi-Analytic F.E. methodadaptation of Semi-Analytic F.E. method
• Validation in the axisymmetric caseValidation in the axisymmetric case
• Transducer diffraction effectsTransducer diffraction effects• influence influence of aof apertureperture // bandwith bandwith in the in the a axisymmetric casexisymmetric case• 2D case2D case: : rectangular cross sectionrectangular cross section
• Summary – Summary – WWorkork in progress in progress
Transducer diffraction effects (axisym.)Transducer diffraction effects (axisym.)
0 d / 2 =12.5mm
t
B-scans at z = 250 mm
axial displacement uz (r,t)
d Øfield points
z
aperture:
Ø = 25 mm200 µs
0 d / 2 =12.5mm
t
aperture:
Ø = 12.5 mm400 µs
0 d / 2 =12.5mm
t
aperture:point-source
960 µs
Transducer diffraction effects (axisym.)Transducer diffraction effects (axisym.)6
.7 %
20
%4
0 %
excitation pulse T and R : 12.5-mm-Øbw
T and R : 25-mm-Ø
Transducer diffraction effects Transducer diffraction effects (2D case)(2D case)• Guide of rectangular cross-section 20x10mm (Steel)• 4 types of modes (2 axes of symmetry)• 11 propagative modes at f=200 kHz
mode shape (Uz):Flexural Y Flexural X Torsional Extensional
500 elements
Transducer diffraction effects (2D case)Transducer diffraction effects (2D case)
Excitation pulse (fc=200kHz, bp=10%) :
Frequency (MHz)
Gro
up v
eloc
ity
(mm
/s) extensional modes
z=1m
circular:Ø = 10 mm
Ø = 10 mm
transducer Etransducer R
S
z dxdytyxv
tO
),,(
)(
rectangular: 20 x 10 mm²
Transducer diffraction effects (2D case)Transducer diffraction effects (2D case)
Rectangular transducer
Circular transducer
• Context of developmentContext of development
• TheoryTheory• brief reviewbrief review• adaptation of Semi-Analytic F.E. methodadaptation of Semi-Analytic F.E. method
• Validation in the axisymmetric caseValidation in the axisymmetric case
• Transducer diffraction effectsTransducer diffraction effects• influence influence of aof apertureperture // bandwith bandwith in the in the a axisymmetric casexisymmetric case• 2D case2D case: : rectangular cross sectionrectangular cross section
• Summary – Summary – WWorkork in progress in progress
Summary – Work in progressSummary – Work in progress
• Summary:
- SAFE method extended to case of transducer mounted on guide section:- can deal with arbitrary guide (geometry, anisotropy) with symmetry of translation- very efficient numerically (computation in the sole section, i.e. 2D or even 1D)- validated by comparison with existing results for cylinder (theo. – exp.)
- importance of transducer diffraction effects:- requires a proper simulation tool to be predicted- easily studied using SAFE computations- as strong here as in the case of radiation from the guiding surface
• Work in progress: - implementation in CIVA
- scattering by a crack normal to the guide axis computed by SAFE- experimental validation of our own
more stuff…
visco-elastic absorbing layervisco-elastic absorbing layer
used to deal with sections of infinite extent:Hooke’s tensor in the absorbing layer has
an increasing (with r) imaginary part
Liu & Achenbach, J. Appl. Mech. (1994)
Transducer diffraction effects: Transducer diffraction effects: embeddeembedded guided guide
rsteel
cement
• axisymmetry: still a 1D computation in the present case• no more real-valued wavenumbers, imaginary parts standing for the leakage of energy in the cement of propagative modes in the steel core.
1
-2.50 a
0
1
-30 a
0
1
-60 a
01
-30 a
0
u z(r)
-2.5
0
-4.50 a
1.2
-0.20 a
0
1
0 a
0
1.5
-30 a
0
u r(r)
L(0,1) L(0,2) L(0,3) L(0,4)471.4 m-1562.1 m-1818.9 m-11049.8 m-1
471.7 – 6.2 i m-1561.7 – 14.6 i m-1819.0 – 8.5 i m-11045.6 – 34.6 i m-1
at z=0, 500 kHz – steel cylinder: free – embedded in cement
Transducer diffraction effects: Transducer diffraction effects: embeddeembedded guided guide
transducer E cylindrical guide transducer R= transducer E
Ø2a
Transducer diffraction effectsTransducer diffraction effects:: apertureaperture
otherwise,0)(
,1)(
rA
arrA
otherwise,0)(
2/,1)(
rA
arrA
araa
ar
rA
arrA
2/,2
)2(cos1
)(
2/,1)(
receiver output
a
z drrtrvrAtO0
),()()(
Transducer diffraction effectsTransducer diffraction effects:: apertureaperture
-7.5 dB-7.5 dB
-9.3 dB-9.3 dB
ur (r,t) receiver outputaperture uz (r,t)
-9.9 dB-9.9 dB
transducer E cylindrical guide transducer R= transducer E
Ød
Transducer diffraction effectsTransducer diffraction effects:: apertureaperture
otherwise,0)(
2/,1)(
rA
drrA
otherwise,0)(
4/,1)(
rA
drrA
receiver output
2/
0),()()(
d
z drrtrvrAtO
3 excitation pulses :- same center freq.: 1107kHz- 3 bandwidths: 6.7, 20, 40%
• Combination of effects of apperture in transmission and in reception and effects of relative bandwidth
0)( 22 iiii
3i2
i1 dMdKKK kjk
iE
rdr1HT1
i1 BcBK
NLNLB 0r,r1
TMzMrzr ddddp) (mode,,1,1, ...pd
00
00
0
00
10
00
00
011
0
rLLr
)(0)(0)(0
0)(0)(0)()(
321
321
rrr
rrrr
N
000
02
02
02
Hc
mixed end conditions and axisymmetry: direct projection of the modes Duncan Fama, Quart. J. Mech. Appl. Math. (1972)
Herczynski & Folk, Quart. J. Mech. Appl. Math. (1989)
n
zz(n)n(source)zzn
r(n)n(source)r σAσuAu ~and~
orthogonality relation Fraser, J. Sound Vib. (1975)
mnrdruuQ mzznz
a
nrzmrmn ifexcept 0)~~~~(~
)()(
0
)()(
rdruuQ
A rcesouzznz
a
nrzourcesr
nn
n )~~~(~1
)()(
0
)()(
zguide axis
pure end conditions: direct projection impossible
nzz(n)n(source)zz
nrz(n)n
σAσ
σA
~
~0
minimization of residual boundary values at z = 0
Gregory & Gladwell , Quart. J. Mech. Appl. Math. (1989) Puckett & Peterson, Ultrasonics (2005)
Theory: Theory: brief reviewbrief review (contd.)(contd.)
Transducer diffraction effectsTransducer diffraction effects:: apertureaperture
0 d / 2 =12.5mm
t
0 d / 2 =12.5mm
t
0 d / 2 =12.5mm
t
B-scans at z = 250 mm
radial displacement ur (r,t)
d Øfield points
z
aperture:
Ø = 25 mm
aperture:
Ø = 12.5 mm
aperture:point-source
200 µs
400 µs
960 µs
-9.3 dB-9.3 dB
-7.5 dB-7.5 dB
+1.8 dB+1.8 dB
Transducer diffraction effectsTransducer diffraction effects:: apertureaperture
aperture:
Ø = 12.5 mm
aperture:point-source
d Ø
z
received signal
at z = 250 mm
aperture:
Ø = 25 mm
40 60 80 100
µs120 140 160
Theory: Theory: validation validation vs. vs. exact resultsexact results
• Cylindrical case: Pochhammer’s solution for wavenumbers(roots of an exact equation)
here: 1MHz, steel cylinder of 20-mm-Ø – 9 propagative modes
623.5870.4991.51049.41253.61550.51757.61884.32101.930 elts
623.4870.2991.31049.41253.41550.51757.61884.22101.320 elts
619.8866.1988.11047.71247.61548.91757.31884.12094.110 elts
557.1784.1951.41035.81174.21525.91753.11883.12058.45 elts
S.A
.F.E
.
(wavenumbers in m-1)
L(0,9)L(0,8)L(0,7)L(0,6)L(0,5)L(0,4)L(0,3)L(0,2)L(0,1)mode:
623.4870.4991.41049.41253.61550.51757.61884.32102.0exact
0.06 ‰ error 10.6 % with 5 elements 0.1 ‰ error 0.6 % with 10 elements0 % error 0.3 ‰ with 20 elements0 % error 0.16 ‰ with 30 elements
Transducer diffraction effectsTransducer diffraction effects
-10
z/Ø
0
-20
-30
-40
-50
-60
0.2 0.4 0.6 0.8 10
ampl
itude
in d
B
• Amplitude variation (z) of propagative, evanescent and inhomogeneous modes with imaginary part < 1500 m-1 as radiated in the previous configuration
at z = 250mm, only thepropagative modes contribute to the receivedsignal
Transducer diffraction effects: Transducer diffraction effects: excitation spectrumexcitation spectrum
• Same center frequency, 3 different bandwidths
6.7
%2
0 %
40
%
excitation pulse simulated received signalbw