Cara Menganalisa Kekuatan Material Dengan ANSYS

CARA MENGGAMBAR DENGAN MENGGUNAKAN PROGRAM ANSYS

Tahapan ahapan-tah -tahapa apan n nya nya : 1. Membuka program ansys > pilih geometry klik 2 kali 2. Tampillah Tampillah menu selanjut seperti di bawah ini,selanjut ini,sela njut klik ok

3. elanjutnya pilih model kemudian klik !" plane lalu klik kanan pilih menu look at

#. $iih sket%hing > re%tangle > dimensions > hori&ontal > 'ertikal > draw > line ( garis segitiga) > modi*y > trim ( untuk memotong garis segitiga)

+. pilih menu etrude > generate

. $ilih menu proje%t > simulation > new analisis > klik ok

. /lik mesh > klik kanan > generate mesh

0. /lik menu *a%e > stati% stru%tural > klik kanan > *or%e

. klik menu sol'e > solution > eui'alent stress

1. klik solution > maimum shear stress

11. klik solution > total de*ormation

HASIL DATA YANG DI DAPAT

Project First Saved Wednesday, January 11, 2012 Last Saved Wednesday, January 11, 2012 Product Version

11.0 SP1 Release

Contents 

Model o

4eometry 

olid

o

Mesh

o

Static Structural



5nalysis ettings



6oads



olution 

olution 7n*ormation



8esults



Ma 9ui'alent tress 



Ma hear tress 



8esults

8esults

Material Data o

tru%tural teel

Units TABLE 1 Unit System Metric m, !", #, $%, s, V, &' &n"le

(e"rees

Rotational Velocity

rad)s

Model Geometry TABLE 2 Model > Geometry *+ect #ame State

Geometry Fully (e-ined

Definition Source (/!ulia/&#SS/Proect.a"d+

3y4e

(esi"nModeler

Len"t Unit 5lement %ontrol

Millimeters Pro"ram %ontrolled

(is4lay Style

Part %olor

Bounding Box Len"t 6

0,1 m

Len"t 

,e7002 m

Len"t 8

9,e7002 m

Properties Volume

1,1e700 m:

Mass

0,;<< !"

Statistics =odies

1

&ctive =odies

1

#odes

9<>1

5lements

?

Preferences @m4ort Solid =odies

es

@m4ort Sur-ace =odies

es

@m4ort Line =odies

es

Parameter Processin"

es

Personal Parameter Aey

(S

%&( &ttri+ute 3rans-er

#o

#amed Selection Processin"

#o

Material Pro4erties 3rans-er

#o

%&( &ssociativity

es

@m4ort %oordinate Systems

#o

Reader Save Part File

#o

@m4ort Usin" @nstances

es

(o Smart U4date

#o

&ttac File Via 3em4 File

#o

&nalysis 3y4e

97(

MiBed @m4ort Resolution

#one

5nclosure and Symmetry Processin"

es

TABLE 3 Model > Geometry > Parts *+ect #ame State

Solid Mesed

Graphics Properties Visi+le 3rans4arency

es 1

Definition Su44ressed

#o

Material Structural Steel

Sti--ness =eavior

FleBi+le

#onlinear Material 5--ects

es

Bounding Box Len"t 6

0,1 m

Len"t 

,e7002 m

Len"t 8

9,e7002 m

Properties Volume

1,1e700 m:

Mass

0,;<< !"

%entroid 6 7C,20>e700> m %entroid  7?,01?Ce700 m %entroid 8

1,Ce7002 m

Moment o- @nertia @41

1,;2;>e700 !"DmE


;,C199e700 !"DmE


;,<<
Statistics #odes

9<>1

5lements

?

Mesh TABLE 4 Model > Mesh *+ect #ame State

Mesh Solved

Defaults Pysics Pre-erence Relevance

Mecanical 0

Advanced Relevance %enter

%oarse

5lement Sie

(e-ault

Sa4e %ec!in" Standard Mecanical Solid 5lement Midside #odes Pro"ram %ontrolled Strai"t Sided 5lements @nitial Sie Seed

#o &ctive &ssem+ly

Smootin"

LoG

3ransition

Fast

Statistics #odes

9<>1

5lements

?

Static Structural TABLE 5 Model > Analysis *+ect #ame Static Structural State

Fully (e-ined

Definition Pysics 3y4e

Structural

&nalysis 3y4e Static Structural Options Re-erence 3em4

22,

%$TABLE 6 Model > Sta Str!t!ral > Analysis Se"n#s *+ect #ame

Analysis Settings

State

Fully (e-ined Step Controls

#um+er *- Ste4s

1,

%urrent Ste4 #um+er

1,

Ste4 5nd 3ime &uto 3ime Ste44in"

1, s Pro"ram %ontrolled Solver Controls

Solver 3y4e

Pro"ram %ontrolled

Wea! S4rin"s

Pro"ram %ontrolled

Lar"e (e-lection

*--

@nertia Relie-

*-- Nonlinear Controls

Force %onver"ence

Pro"ram %ontrolled

Moment %onver"ence

Pro"ram %ontrolled

(is4lacement %onver"ence

Pro"ram %ontrolled

Rotation %onver"ence

Pro"ram %ontrolled

Line Searc

Pro"ram %ontrolled Output Controls

%alculate Stress

es

%alculate Strain

es

%alculate Results &t

&ll 3ime Points Analysis Data Manageent

Solver Files (irectory (/!ulia/&#SS/Proect Simulation Files/Static Structural/ Future &nalysis

#one

Save &#SS d+

#o

(elete Unneeded Files

es

#onlinear Solution

#o TABLE $ Model > Sta Str!t!ral > Loads

*+ect #ame State

Force

Force 2 Fully (e-ined

Scope Sco4in" Metod Heometry

Heometry Selection 1 Face Definition

(e-ine =y 3y4e

%om4onents Force

6 %om4onent 1000, # ram4ed' 71000, # ram4ed'  %om4onent

0, # ram4ed'

8 %om4onent

0, # ram4ed'

Su44ressed

#o

!"GU#$ % Model & Static Structural & !orce

!"GU#$ ' Model & Static Structural & !orce '

Solution TABLE % Model > Sta Str!t!ral > Sol!on *+ect #ame Solution State Solved Adaptive Mesh #efineent MaB Re-inement Loo4s

1,

Re-inement (e4t

2,

TABLE & Model > Sta Str!t!ral > Sol!on > Sol!on 'n(ormaon *+ect #ame Solution Information State

Solved

Solution "nforation Solution *ut4ut #eGton7Ra4son Residuals

Solver *ut4ut 0

U4date @nterval

2,C s

(is4lay Points

&ll

TABLE 1) Model > Sta Str!t!ral > Sol!on > *es!lts *+ect #ame

Equivalent Stress

Maximum Shear Stress Total Deformation

State

Solved Scope

Heometry

&ll =odies Definition

3y4e 5Iuivalent von7Mises' Stress MaBimum Sear Stress 3otal (e-ormation (is4lay 3ime

5nd 3ime #esults

Minimum

20;< Pa

11;02 Pa

2,?;>
MaBimum

>,<1<2e00> Pa

9,;0;e00> Pa

1,11??e700> m

"nforation 3ime

1, s

Load Ste4

1

Su+ste4

1

@teration #um+er

1 TABLE 11 Model > Sta Str!t!ral > Sol!on > Stress Sa(ety Tools *+ect #ame

Max Equivalent Stress

State

Solved

Definition 3eory

MaB 5Iuivalent Stress

Stress Limit 3y4e 3ensile ield Per Material TABLE 12 Model > Sta Str!t!ral > Sol!on > Ma+ E,!i-alent Stress > *es!lts *+ect #ame Safety Factor Safety Margin State

Solved Scope

Heometry


3y4e Sa-ety Factor Sa-ety Mar"in (is4lay 3ime

5nd 3ime #esults

Minimum

K 10

K<

"nforation 3ime

1, s

Load Ste4

1

Su+ste4

1

@teration #um+er

1

TABLE 13 Model > Sta Str!t!ral > Sol!on > Stress Sa(ety Tools

*+ect #ame

Max Shear Stress

State

Solved

Definition 3eory

MaB Sear Stress

Factor

0,C

Stress Limit 3y4e 3ensile ield Per Material TABLE 14 Model > Sta Str!t!ral > Sol!on > Ma+ Shear Stress > *es!lts *+ect #ame Safety Factor Safety Margin State

Solved Scope

Heometry


3y4e Sa-ety Factor Sa-ety Mar"in (is4lay 3ime

5nd 3ime #esults

Minimum

K 10

K<

"nforation 3ime

1, s

Load Ste4

1

Su+ste4

1

@teration #um+er

1

Material Data Structural Steel (AB)$ %* Structural Steel & Constants Structural oun"s Modulus

2,e011 Pa

Poissons Ratio

0,9

(ensity

?;C0, !")m:

3ermal 5B4ansion

1,2e700C 1)

%$3ensile ield Stren"t

2,Ce00; Pa

%om4ressive ield Stren"t

2,Ce00; Pa

3ensile Ultimate Stren"t

,>e00; Pa

%om4ressive Ultimate Stren"t

0, Pa

(heral 3ermal %onductivity

>0,C W)mD

%$S4eci-ic eat

9, J)!"D

%$$lectroagnetics Relative Permea+ility

10000

Resistivity 1,?e700? *mDm

!"GU#$ + Structural Steel & Alternating Stress

TABLE 16 Str!t!ral Steel > Alternan# Stress > Pro.erty A/ri0!tes @nter4olation

Lo"7Lo"

Mean %urve 3y4e Mean Stress TABLE 1$ Str!t!ral Steel > Alternan# Stress > Alternan# Stress !r-e ata Mean Value Pa 0, TABLE 1% Str!t!ral Steel > Alternan# Stress > Alternan# Stress -s yles %ycles

<ernatin" Stress Pa

10,

9,<<
20,

2,;2?e00<

C0,

1,;<>e00<

100,

1,19e00<

200,

1,0>
2000,

,1e00;

10000

2,>2e00;

20000

2,1e00;

1,e00C

1,9;e00;

2,e00C

1,1e00;

1,e00>

;,>2e00?

!"GU#$ , Structural Steel & Strain-)ife Paraeters

TABLE 1& Str!t!ral Steel > StrainLi(e Parameters > Pro.erty A/ri0!tes (is4lay %urve 3y4e Strain7Li-e TABLE 2) Str!t!ral Steel > StrainLi(e Parameters > StrainLi(e Parameters Stren"t %oe--icient Pa <,2e00; Stren"t 5B4onent

70,10>

(uctility %oe--icient

0,219

(uctility 5B4onent

70,?

%yclic Stren"t %oe--icient Pa 1,e00< %yclic Strain ardenin" 5B4onent

0,2

Cara Menganalisa Kekuatan Material Dengan ANSYS

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