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Simulation of part

analisa 3

Date: 16 Januari 2016

Designer: Solidworks

Study name:Study 1 C45

Analysis type:Static

Table of ContentsDescription...........................................1Assumptions..........................................2Model n!ormation..................................2Study "roperties.....................................#$nits..................................................#Material "roperties.................................4%oads and &i'tures..................................4Mes( n!ormation....................................5)esultant &orces....................................6

Study )esults........................................*Conclusion............................................+

Description,o Data

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Assumptions

Model Information

Model name: part analisa 3

Current Configuration: Default

Solid Bodies

Document Name andReference

Treated As olumetric !roperties Document !at"#DateModified

Boss$%&trude'

Solid Body

Mass:()*+,(' -g

olume:.)...(/..,( m03

Density:1+.. -g#m03

2eig"t:(*),, N

D:4tugas4pro5ect

ali45ig4part analisa

3)S6D!RT

7an (' (:,/:*' ,.('

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Study !roperties

Study name Study 1 C45

Analysis type Static

Mes" type Solid Mes(

T"ermal %ffect: /n

T"ermal option nclude temperature loads8ero strain temperature 2+ elin

Include fluid pressure effects from Solid2or-s

9lo Simulation

/!!

Sol;er type &&3"lus

Inplane %ffect: /!!

Soft Spring: /!!

Inertial Relief: /!!

Incompatible bonding options Automatic

6arge displacement /!!

Compute free body forces /n

9riction /!!

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Material !roperties

Model Reference !roperties Components

Name: 1.050# C459Model type: %inear 3lastic sotropic

Default failure

criterion:

Ma' on Mises Stress

=ield strengt": 5.e

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Mes" Information

Mes" type Solid Mes(

Mes"er

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Resultant 9orces

Reaction 9orces

Selection set

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Study Results

Name Type Min Ma&

Stress1 /, on Mises Stress 0.0015+4*4 ,:mm;2 M"a9

,ode 44

116.66# ,:mm;2 M"a9

,ode 12040

part analisa 3$Study ( C*$Stress$Stress(

Name Type Min Ma&Displacement1 $)3S )esultant Displacement 0 mm,ode +

0.04624+ mm

,ode 22

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Name Type Min Ma&

part analisa 3$Study ( C*$Displacement$Displacement(

Name Type Min Ma&

Strain1 3S), 3uialent Strain .+6++*e=00+

3lement 6*+

0.0004#*+6

3lement 15+4

part analisa 3$Study ( C*$Strain$Strain(

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Name Type Min Ma&

&actor o! Sa!ety1 Ma' on Mises Stress 4.+*15

,ode 12040

#6#6+5

,ode 44

part analisa 3$Study ( C*$9actor of Safety$9actor of Safety(

Conclusion

Analy-ed wit( Solidorks Simulation Simulation o! part analisa # +