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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
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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
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RESULT
Thus the Stress Analy3ing for Rectangular Plate with $ircular 4ole is $arried *ut(
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STRESS ANALYSIS ON L-BRACET
Ex.No:0!
Date:
AIM
To Analysis the stress on ,racket
%*DE&'!
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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 > -./-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(
&oad > Define load > Apply > Structural > Displacement > *n area > Select
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(
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RESULT
Thus the Stress Analysis on :&; ,racket is $arried *ut
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ANALYSIS BEAM
"S#$%&' S(%%o)te* Bea$+
Ex.No:0,Date:
AIM
To shear force and ending moment of ,eam for the analy3ing
%*DE&'!
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PROCEDURE
Preference > Structure >ok
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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RESULT
Thus the analysis of the ,eam is $arried *ut
ANALYSIS BEAM
"Cat#&ee) Bea$+
Ex.o:0/
Date:
AIM
To shear force and ending moment of ,eam for the analy3ing
%*DE&'!
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PROCEDURE
Preference > Structure
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(
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%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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RESULT
Thus the analysis of the ,eam is $arried *ut
ANALYSIS BEAM
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"F#xe* Bea$+
Ex.o:0
Date:
AIM
To shear force and ending moment of ,eam for the analy3ing
%*DE&'!
PROCEDURE
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Preference > Structure
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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RESULT
Thus the analysis of the ,eam is $arried *ut
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STRESS ANALYSISEx.No:01
Date:
A'%
To analysis the stress
%*DE&'!
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PR*$EDRE
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 > *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
%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
$heck the stress Analysis
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RES&T
Thus the analysis the Stress and $arried *ut
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HEAT CONDUCTION ANALYSIS ON HOLLOW CYLINDER
Ex.No:0
Date:
AimB
To analysis on heat conduction of hollow cylinder of the ansys software
%*DE&'!
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PR*$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 > $ounter plot > Element Result > 4eat flow >ok
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ResultB
Thus we analysis on heat conduction of hollow cylinder of the ansys software
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HEAT CON3ECTION ANALYSIS ON HOLLOW CYLINDER
Ex.No:04
Date:
AimB
To analysis on heat con1ection of hollow cylinder of the ansys software(
%*DE&'!
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PR*$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
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ResultB
Thus we analysis on heat con1ection of hollow cylinder of the ansys software
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HARMONIC ANALYSIS ON BEAM
Ex.No:50
Date:
AIM
To Analysis of 4armonic ,eam
%*DE&'!
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PROCEDURE
Preference > Structure >ok
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
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RESULTThus the analy3ing of 4armonic eam is $arried *uts
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MODE FRE6UENCY ANALYSIS OF BEAMS.
"$antile1er ,eam)Ex.No:55
Date:
AIM
To Analysis of %ode fre@uency Analysis of $antile1er ,eam
%*DE&'!
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PROCEDURE
Preference > Structure >ok
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
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RESULT
Thus the analy3ing of %ode fre@uency of $antile1er eam is $arried *uts
BEYOND
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SYLLABUS
MODELLING USING A7ISYMMETRY
Ex.No:52
Date:
AIM
To determine the stress analysis of ais symmetry component
%*DE&'!
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PROCEDURE
Preference > Structure > ok
Preprocessor > Element Type > Add/Edit/Delete > Add > Solid >Triangle6
noded 2 > *k > *ption >Select aissymmetic> *k
%aterial prop > %aterial model > Structure > &inear > Elastic > 'sotropic >
2# > Poisson ratio > () > *k
%odeling > $reate > Area > Rectangle >,y dimension > Apply >.#-2--. > Apply > -2-"#-.> *k
%eshing > %esh tool > Select the o0ect
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&oad > Define load > Apply > Structural > Displacement > Symmetric ,($ >
*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
Solution > Sol1e > $urrent &S > *k
eneral Post Pros > Plot Result > $ounter Plot > !odal >*k
$heck the stress Analysis
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RES&T
Thus the stress analysis of ais symmetry component is $arried *ut