ansys lab record experiments-april-2012

5/25/2018 Ansys Lab Record Experiments-April-2012

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STRESS ANALYSIS FOR RECTANGULAR PLATE WITH

CIRCULAR HOLE

Ex.No:02

Date:

AIM

To analysis the Stress Rectangular plate with circular hole

MODELING


2/39

PROCEDURE

Preference > Structure > ok

Preprocessor > Element Type > Add/Edit/Delete > Add > Solid >2 !ode "# >

$lose

%aterial prop > %aterial model > Structure > &inear > Elastic > 'sotropic >

2# > Poisson ratio > () > *k

%odeling > $reate > +olume > ,lock >,y dimension > -./-#/-.

>$ylinder > Solid cylinder > #-2#-.#-2

%odeling > *peration > ,ooleans >Sutract > Select the *0ect> *k

%eshing > %esh tool > Select the o0ect

&oad > Define load > Apply > Structural > Displacement > *n area > Select

the o0ect > *k

Pressure > *n area > Select the o0ect > *k

Solution > Sol1e > $urrent &S > *k

eneral Post Pros > Plot Result > $ounter Plot > !odal >*k

Plot $ontrols > Animate >$heck the stress Analysis


3/39

RESULT

Thus the Stress Analy3ing for Rectangular Plate with $ircular 4ole is $arried *ut(


4/39

STRESS ANALYSIS ON L-BRACET

Ex.No:0!

Date:

AIM

To Analysis the stress on ,racket

%*DE&'!


5/39

PROCEDURE

Preference > Structure >ok


$lose



%odeling > $reate > +olume > ,lock >,y dimension > -./-5/-.# >

Apply > ,y dimension > 6-./-76/-.# > *k(> $ylinder > Solid $ylinder

> -2-2-.# > Apply > Solid $ylinder > 8-76-2-.# > Apply > Solid

$ylinder >-2-9(#-2> Apply >8-76-9(#-2> *k(

*perate > ,ooleans > Add> +olume > Select the *0ect > *k > Sutract >

+olume > Pick the Solid *0ect> *k(

%eshing > %esh tool > +olume > %esh > Select the o0ect > *k(


the *0ect > *k(

Pressure > *n area > Select the o0ect >. > *k(

Solution > Sol1e > $urrent &S > *k(

eneral Post Pros > Plot Result > $ounter Plot > !odal >*k(

+iew the Animation(


6/39

RESULT

Thus the Stress Analysis on :&; ,racket is $arried *ut


7/39

ANALYSIS BEAM

"S#$%&' S(%%o)te* Bea$+

Ex.No:0,Date:

AIM

To shear force and ending moment of ,eam for the analy3ing

%*DE&'!


8/39

PROCEDURE


Preprocessor > Element type >Add/Edit/Delete/ > ,eam > 2Elastic ) > *k(

Real $onst > Add > ok > i1e the dimension 1alue > *k(

%aterial Prop > %aterial model > Structural > &inear > Elastic > 'sentropic >

E< =2# > PR $reate > ?ey point > 'n acti1e $S > *k > &ine > Straight &ine >

$onnect two point > *k(

%eshing > %esh tool > &ine > %esh > Select the *0ect > *k(

&oad > Define &oad > Apply > Structure >Displacement > *n key points >*k(

Pressure > *n eam > Select the ,eam > i1e the dimension the 1ale > *k(

Solution > Sol1e > $urrent &S > Solution Done > *k(

eneral Post Pros > Element tale > Define tale > Add > ,y se@uence

!umer > !%'S$> ./)/2/5 >*k(

Plot Result > $ounter plot > &ine tale element > ,y se@uence !umer >

!%'S$> ./)/2/5 >*k(


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11/39

RESULT

Thus the analysis of the ,eam is $arried *ut

ANALYSIS BEAM

"Cat#&ee) Bea$+

Ex.o:0/

Date:

AIM


%*DE&'!


12/39

PROCEDURE

Preference > Structure







13/39






!umer > !%'S$> ./)/2/5 >*k(


!%'S$> ./)/2/5 >*k(


14/39

RESULT


ANALYSIS BEAM


15/39

"F#xe* Bea$+

Ex.o:0

Date:

AIM


%*DE&'!

PROCEDURE


16/39

Preference > Structure











!umer > !%'S$> ./)/2/5 >*k(


!%'S$> ./)/2/5 >*k(


17/39

RESULT



18/39

STRESS ANALYSISEx.No:01

Date:

A'%

To analysis the stress

%*DE&'!


19/39

PR*$EDRE



$lose



%odeling > $reate > +olume > ,lock >,y dimension > -##/-#/-.#

>$ylinder > Solid cylinder > ##-2#-2#-.#

%odeling > *perate > ,oolean > Add > +olume > Select the o0ect > *k

%odeling > $reate > +olume > Solid $ylinder >,y dimension >##-2#-.#-2>

%odeling > *perate > ,oolean > Sutract >+olume > Select the *0ect> *k



the o0ect > *k

Pressure > *n area > Select the o0ect > *k



$heck the stress Analysis


20/39

RES&T

Thus the analysis the Stress and $arried *ut


21/39

HEAT CONDUCTION ANALYSIS ON HOLLOW CYLINDER

Ex.No:0

Date:

AimB

To analysis on heat conduction of hollow cylinder of the ansys software

%*DE&'!


22/39

PR*$EDREB

Preferences > Thermal >ok

Preprocessor> Element type >Add/Edit/Delete > Add >Solid > 2!odes "# >ok

%etrical prop > Thermal >$onducti1ity >'sotropic > ?create >+olume >$ylinder > hollow cylinder > mesh tool >+olume >mesh >pick the solid >ok

&oad >Analysis type >!ew analysis >ok

&oad >define load >Apply >Temperature *n node > ok

Solution >sol1e>$urrent &S >Solution done >ok

eneral post proc > plot result > $ounter plot > Element Result > 4eat flow >ok


23/39

ResultB

Thus we analysis on heat conduction of hollow cylinder of the ansys software


24/39

HEAT CON3ECTION ANALYSIS ON HOLLOW CYLINDER

Ex.No:04

Date:

AimB

To analysis on heat con1ection of hollow cylinder of the ansys software(

%*DE&'!


25/39

PR*$EDREB

Preferences > Thermal >ok

Preprocessor> Element type >Add/Edit/Delete > Add >Solid > 2!odes "# >ok

%etrical prop > Thermal >$onducti1ity >'sotropic > ?create >+olume >$ylinder > hollow cylinder > mesh tool >+olume >mesh >pick the solid >ok

&oad >Analysis type >!ew analysis >ok

&oad >define load >Apply >Temperature *n node > ok

Solution >sol1e>$urrent &S >Solution done >ok

eneral post proc > plot result > $ounter plot > Element Result > 4eat flow >ok


26/39

ResultB

Thus we analysis on heat con1ection of hollow cylinder of the ansys software


27/39

HARMONIC ANALYSIS ON BEAM

Ex.No:50

Date:

AIM

To Analysis of 4armonic ,eam

%*DE&'!


28/39

PROCEDURE


Preprocessor > Element tale > Add/Edit/Delete > ,eam >2D Elastic ) > *k

Real constant > Add > *k > i1e the dimensions

%aterial props > %aterial model > Structural > &inear > Elastic > 'sentropic > *k

Density > i1e the Dimension > *k

%odeling > $reate > ?ey point > 'n acti1e $S > *k > &ines > &ine > Straight line > Pick

point > *k

%eshing > %esh tool > &ines > %esh >*k

&oads > Define &oad > Apply > Structural > Displacement > *n key points > *k >

Corce/%oment > *n nodes > i1e the dimension > *k

Solution > Analysis type > !ew analysis > 4armonic > *k

Solution > Analysis *ption > full > Real imaginary > spares sol1er >*k

Solution > &oad step option > Time/fre@uency> fre@uency and susteps>stepped>*k

Solution > sol1e > $urrent &S > *k

Time &ist Post pros > +ariale 1iewer > Add Data > *k


29/39


30/39

RESULTThus the analy3ing of 4armonic eam is $arried *uts


31/39

MODE FRE6UENCY ANALYSIS OF BEAMS.

"$antile1er ,eam)Ex.No:55

Date:

AIM

To Analysis of %ode fre@uency Analysis of $antile1er ,eam

%*DE&'!


32/39

PROCEDURE


Preprocessor > Element tale > Add/Edit/Delete > ,eam >2D Elastic ) > *k

Real constant > Add > *k > i1e the dimensions

%aterial props > %aterial model > Structural > &inear > Elastic > 'sentropic > *k

Density > i1e the Dimension > *k

%odeling > $reate > ?ey point > 'n acti1e $S > *k > &ines > &ine > Straight line > Pick

point > *k

%eshing > %esh tool > &ines > %esh >*k

&oads > Define &oad > Apply > Structural > Displacement > *n key points > *k

Solution > Analysis type > !ew analysis > %odal > *k

Solution > Analysis *ption > ,lock &anc3os>

!o(of mode to Etract = .Epand mode shapes = es

!%*DE !o(of mode epand=. > ok

,lock &anc3os methodF > CREG, start = - CREG, end = -

!umer !ormal '3emode shape= To mass matri

Solution > sol1e > $urrent &S > *k

eneral post process> Result summary >ok>close

Read results >$he@ueFCirst step -second step -Third step >ok

Plot Results > contour plot >!odal solution >Dof solution > Displacement of +ector sum >

Plot controls >style >si3e and shape = percent- Displacement of element= on >ok

Read results = Cirst step-second step-Third stepHindow I Right click ReplotF>ok

Plot controls > Animate>Deformed Results >Dof solution >Translation ok


33/39


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35/39

RESULT

Thus the analy3ing of %ode fre@uency of $antile1er eam is $arried *uts

BEYOND


36/39

SYLLABUS

MODELLING USING A7ISYMMETRY

Ex.No:52

Date:

AIM

To determine the stress analysis of ais symmetry component

%*DE&'!


37/39

PROCEDURE

Preference > Structure > ok

Preprocessor > Element Type > Add/Edit/Delete > Add > Solid >Triangle6

noded 2 > *k > *ption >Select aissymmetic> *k



%odeling > $reate > Area > Rectangle >,y dimension > Apply >.#-2--. > Apply > -2-"#-.> *k



38/39

&oad > Define load > Apply > Structural > Displacement > Symmetric ,($ >

*n &ine > Select the *0ect > *k

&oad > Define &oad > Apply >Corce/%oment > *n !odes > select the *0ect

> Select C- . > Apply > Select the o0ect > Select C - 7.> *k

&oad > Define load > Apply > Structural > Displacement > *n !odes > Select

the middle o0ect > *k



$heck the stress Analysis


39/39

RES&T

Thus the stress analysis of ais symmetry component is $arried *ut

ansys lab record experiments-april-2012

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