basic beam analysis example2

8/9/2019 Basic Beam Analysis Example2

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Eutectic Metal

Simulation of Part1

Date: November-15-14

Designer: Mahfuzul Haque

Study name: Static 1

Analysis type: Static

Table of ContentsDescription...........................................1Assumptions..........................................

Mo!el "nformation..................................Stu!# $roperties.....................................%&nits..................................................4Material $roperties.................................4'oa!s an! (i)tures..................................5*onnector Definitions..............................+*ontact "nformation................................+Mesh "nformation....................................,Sensor Details........................................,esultant (orces..................................../eams.................................................0Stu!# esults.......................................1*onclusion..........................................11

DescriptionNo Data

Anal#ze! 2ith Soli!3ors Simulation Simulation of $art1 1


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Eutectic Metal Mahfuzul Haque151114

Assumptions

Anal#ze! 2ith Soli!3ors Simulation Simulation of $art1


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Anal#ze! 2ith Soli!3ors Simulation Simulation of $art1 %


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Model Information



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Model name: Part1

Current Configuration: Default

Beam Bodies:Document ame and

!eference"ormulation Properties

Document Pat#$Date

Modified

Beam%1&Boss%E'trude1(

Beam ) *niform C$S

Section Standard%CustomSection Area: +,-./0in23

4engt#:1310/3mm

5olume:./..6-106-m2+

Mass Density:3-..7g$m2+

Mass:13/-637g

8eig#t:136/,--

Beam%3&Boss%E'trude3(

Beam ) *niform C$S

Section Standard%Custom

Section Area: +,-./0in23

4engt#:1310/3mm

5olume:./..6-106-m2+

Mass Density:3-..7g$m2+

Mass:13/-637g

8eig#t:136/,--

Beam%+&Boss%E'trude+( Section Standard%Custom

Section Area: +,-./0in23

4engt#:1936mm



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Study PropertiesStudy name Static 1

Analysis type Static

Mes# type /eam Mesh

Soler type ((6$lus

Inplane Effect: 7ff

Soft Spring: 7ff

Inertial !elief: 7ff

Incompatible bonding options Automatic

4arge displacement 7ff Compute free body forces 7n

!esult folder Soli!3ors !ocument

8c9:users:mahfuz;1:app!ata:local:temp<

*nits

*nit system: S" 8M=S<

4engt#$Displacement mm

Temperature =elvin

Angular elocity a!sec

Pressure$Stress Nm>

Anal#ze! 2ith Soli!3ors Simulation Simulation of $art1 +


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Material Properties

Model !eference Properties Componentsame: 1+ Allo#

Model type: 'inear 6lastic "sotropicDefault failure

criterion:

Ma) von Mises Stress

;ield strengt#: .,5,4e?, Nm>Tensile strengt#: +.0%5+e?, Nm>Elastic modulus: +.0e?1 Nm>

Poisson%

S#ear modulus: .,e?1 Nm>T#ermal e'pansion

coefficient:

.4e-5 =elvin

Soli!/o!# 18/oss-6)tru!e1<

8$art1


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4oads and "i'tures

"i'ture name "i'ture Image "i'ture Details

Immoable%1

Entities: 1 Boint8s<Type: "mmovable 8No translation<

!eference=eometry%1

Entities: 1 Boint8s<!eference: (ront $lane

Type: &se reference @eometr#

Translation: --- !otation: --- --- ---

*nits: in ra!

4oad name 4oad Image 4oad Details

"orce%1

Entities: 1 plane8s


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Connector DefinitionsNo Data

Contact InformationNo Data



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Mes# Information

Mes# type /eam Mesh

Mes# Information % Details

Total odes %

Total Elements 10

Time to complete mes##>mm>ss(: 991

Computer name: MAHCHA3=

Sensor DetailsNo Data



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!esultant "orces

!eaction "orcesSelection set *nits Sum ? Sum ; Sum @ !esultant

6ntire Mo!el N -.4+04+e-% %11%.,+ -%.,0%e-+ %11%.,+

!eaction Moments

Selection set *nits Sum ? Sum ; Sum @ !esultant

6ntire Mo!el N.m 1e-%%



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Beams

Beam "orcesBeam

ameoints A'ial&( S#ear1&( S#ear3&( Moment1&/m( Moment3&/m( Torue&/m(

Beam%

1&Boss%

E'trude1(

11.,55e-

%41.+0%0

-.,4%,e-

1.+0+e- .11404 +.45e-1,

-

1.4++e-

4

-41.+0%01.+05e-

,-1.1+e-+ -5.4% 5.1%e-1+

Beam%

3&Boss%

E'trude3(

11.,55e-

%4.5

-4.4+1e-

+1.51e-+ 5.51 1.+051e-15

5.,,0e-

4-4.5

4.4+4%5e-

+-+.+4e-5 -54.15 -1.%%440e-15

Beam%

+&Boss%

E'trude+(

11.4%+%e-

4-1111.%

-1.4+4,e-

++.0+05e-5 54.1+ .,45e-15

-

1.+414e-

15

1111.%-.450e-

+-.,445e-5 -4,.%0 -1.0,0e-15

Beam%

6&Boss%

E'trude6(

1%.411e-

%

-

.,%

-.10+0e-

-1.0+5,1e-0 -%.451e-5 -1.,0%0e-15

-

1.11+0e-

14

-1111.,+1.050e-

+.01e-5 4,.% -1.%04e-14

Beam Stresses

Beam ame oints A'ial&$m23(Bending

Dir1&$m23(

Bending

Dir3&$m23(

Torsional

&$m23(

8orst

Case&$m23(

Beam%1&Boss%

E'trude1(

1 4.541+%e-1 .%,,5 -.%%, 1.4+1%5e-1 .%%,4,

%.1051e- .%,1%1 -1.%41e?+ 1.%+%e-11 1.%41e?+

Beam%3&Boss%

E'trude3(

1 4.541+4e-1 .5+,15 -1.%4%,e?+ %.0++0e-11 1.%4%,e?+

-1.51++e-1 1.4015 -5.1,15e?,-%.15e-

115.1,15e?,

Beam%+&Boss%

E'trude+(

1 %.1,e- 1.+% -5.1,1+e?, 4.40+e-11 5.1,1+e?,

4.144e-1% .+%05% -1.,%,e?,-4.+1104e-

111.,%,e?,

Beam%6&Boss%

E'trude6(

1 -.14++e-1 5.00,,5e-5 -.+0+45 -4.10,4,e-11

.+0,5

-.0,,e-1 .+1%4 -1.,%+e?, -%.+4e-1 1.,%+e?,



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Study !esults

ame Type Min Ma'

Stress1 S9 Normal Stress -4.,+e-1+ psi

6lement9 10

+.14e-1, psi

6lement9 0

Part1%Static 1%Stress%Stress1

ame Type Min Ma'

Displacement1 &6S9 esultant Displacement ft

No!e9 45

.,%41 ft

No!e9 145

Anal#ze! 2ith Soli!3ors Simulation Simulation of $art1 1%


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ame Type Min Ma'

Part1%Static 1%Displacement%Displacement1

Conclusion


basic beam analysis example2

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