Truss 2D-1 Right Result

8/18/2019 Truss 2D-1 Right Result

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Eutectic Metal

Simulation of Truss2D-1FEA

Date: November-02-14

Designer: Mahfuzul Haque

Study name: Static 2

Analysis type: Static

Table of ContentsDescription...........................................1ssumptions..........................................2Mo!el "nformation..................................2Stu!# $roperties.....................................%&nits..................................................4Material $roperties.................................4'oa!s an! (i)tures..................................*+onnector Definitions..............................*+ontact "nformation................................,Mesh "nformation....................................Sensor Details........................................esultant (orces..................................../eams................................................./Stu!# esults........................................+onclusion..........................................10

DescriptionNo Data

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Eutectic Metal Mahfuzul Haque0271172014

Assumptions



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Model nformation



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Model name: Truss2D-1FEA

Current Configuration: Default

!eam !odies:

Document "ame and#eference

Formulation $roperties Document $at%&DateModified

!eam-1'!oss-E(trude1)

!eam * +niform C&S

Section Standard-Custom

Section Area: ,1../2in02

engt%:23mm

4olume:563,/5e-66.m0,

Mass Density:77668g&m0,

Mass:66.1/,578g

9eig%t:6.6.///"

C:+sersMa%fu;ul


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Study $ropertiesStudy name Static 2

Analysis type Static

Mes% type eam Mesh

Sol>er type ((6$lus

nplane Effect: 8ff

Soft Spring: 8ff

nertial #elief: 8ff

ncompatible bonding options utomatic

arge displacement 8ff Compute free body forces 8n

#esult folder Soli!3ors !ocument 9+:;&sers;Mahfuzul

Haque;Documents;(inite nal#sis<

+nits

+nit system: S" 9M=S<

engt%&Displacement mm

Temperature =elvin

Angular >elocity a!7sec

$ressure&Stress N7m>2

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Material $roperties

Model #eference $roperties Components"ame: llo# Steel

Model type: 'inear 6lastic "sotropicDefault failure

criterion:

Ma) von Mises Stress

?ield strengt%: ,.20422e?00/ N7m>2Tensile strengt%: .2%/2,e?00/ N7m>2Elastic modulus: 2.1e?011 N7m>2

$oisson@s ratio: 0.2/Mass density: 00 @7m>%

S%ear modulus: .e?010 N7m>2T%ermal e(pansion

coefficient:

1.%e-00* 7=elvin

Soli!o!# 19oss-6)tru!e1<

95russ2D-1e Data:"&A

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oads and Fi(tures

Fi(ture name Fi(ture mage Fi(ture Details

Fi(ed-,

Entities: 2 Boint9s<Type: (i)e! Ceometr#

#eference

eometry-1

Entities: 1 Boint9s<#eference: (ront $lane

Type: &se reference @eometr#Translation: ---A ---A 0#otation: ---A ---A ---

+nits: inA ra!

oad name oad mage oad Details

Force-1

Entities: 1 plane9s


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Connector DefinitionsNo Data

Contact nformation

Contact Contact mage Contact $roperties

Clobal +ontact

Type: on!e!Components: 1 component9s<

Bptions: +ompatible

mesh

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Mes% nformation

Mes% type eam Mesh

Mes% nformation - Details

Total "odes 1/*

Total Elements 1/2

Time to complete mes%'%%mmss): 00:00:01

Computer name: MHH3=

Sensor DetailsNo Data



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#esultant Forces

#eaction ForcesSelection set +nits Sum Sum ? Sum #esultant

6ntire Mo!el N -222.411 0 %.*%*e-0%* 222.411

#eaction Moments

Selection set +nits Sum Sum ? Sum #esultant

6ntire Mo!el N.m -*.21,e-0%% -%.04,*e-0%% 0.0140% 0.0140%

!eams

!eam Forces

!eam

"ameoints A(ial'") S%ear1'") S%ear2'") Moment1'"m) Moment2'"m) Tor=ue'"m)

!eam-

1'!oss-

E(trude1)

1 1/*.2% 0.01,4,% 0 0 0.0004**2 0

2 -1/*.2% -0.01/4/ 0 0 -0.00*44,% 0

!eam-

2'!oss-E(trude2)

1 -1%%.,,, -0.1041,-1.%44,e-

0%10 0.01%,%* 0

2 1%%.,,, 0.1041/-.*,0%,e-

0%00 0.00*44,% 0

!eam Stresses

!eam "ame oints A(ial'"&m02)!ending

Dir1'"&m02)

!ending

Dir2'"&m02)

Torsional

'"&m02)

9orst

Case'"&m02)

!eam-1'!oss-

E(trude1)

1 *./41e?00, -4.2/1/2e-02 -1/210-4.%0/2*e-

02,*./,4e?00,

2 *./41e?00, /.*4%/e-02 -21,,/, 4.%0/%1e-02, ,.0,*//e?00,

!eam-2'!oss-

E(trude2)

1 -4.220e?00, -%.2,41e-02* -*424**-2.1/**e-

024.,%1,e?00,

2 -4.220e?00, -%.4%*//e-02, 21,,/, /.14,/2e-02 4.4%%e?00,



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Study #esults

"ame Type Min Ma(

Stress1 SE: E Normal Stress -,12.1,1 psi

6lement: 10

/4/.%*% psi

6lement: 1

Truss2D-1FEA-Static 2-Stress-Stress1

"ame Type Min Ma(

Displacement1 &6S: esultant Displacement 0 in

No!e: 10

0.000%21*%2 in

No!e: 1



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"ame Type Min Ma(

Truss2D-1FEA-Static 2-Displacement-Displacement1

Conclusion

nal#ze! ith Soli!3ors Simulation Simulation of 5russ2D-1(6 1%