Ansys flat top cylinder with fillet 35 mpa 12 25 version 2
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Transcript of Ansys flat top cylinder with fillet 35 mpa 12 25 version 2
Pressure cylinder with internal filleted radius
Prof. CharltonS. Inao
Defence Engineering University
Bishoftu,Ethiopia
Problem Definition:Find the DMX, maximum displacement ,SMN, minimum
stress and SMX, maximum stress for the gas pressure cylinder subjected to 35 Mpa internal pressure, young’s modulus of elasticity is 200 Gpa, poisson(v) ratio is 0.3. Illustration/figure is provided.
Cylinder Dimension:
Outside Diameter: 200, Height: 400
Inside Diameter: 150
Wall thickness : 25
Fillet Radius: 25
Quarter of a gas pressure cylinder
Half of gas cylinder in 3D wireframe
Preprocessing
Define ElementPreprocessor> Element type>Add>Element type>Solid>Tet
10 Node 187>Ok>Close
Element type=>Solid,Tet 10 Node,187
Solid, Tet 10 Node, 187
Element >Options>Pure Displacement>Ok>Close
Real constants>Solid 187 element type does not require real constants
Apply Material Properties…Preprocessor>Material Props>Material Models>Material Model
No.1>Structural>Linear>Elastic>Isotropic>Input Value for Elasticity and Poisson Ratio
Modulus of Elasticity=2e11 0r 200e9Poisson Ratio= 0.3 normal value for steel,
then click OK
Keypoints x y z1 75 0 2 100 0 3 100 200 4 0 200 5 0 175 6 50 175 7 75 150 8 50 150
Modeling PhaseInput key points in active coordinate
System, the x and y coordinates
Modeling Phase
Your Screen should look like this
Modeling>Create>Lines>Lines>Straight Lines>pick
Pick KP1 and KP22 and 33 and 44and 55 and 6 1 and 7
Creating Straight Lines
Creating Arc ,=>LARC,6,7,8,25
Create area arbitrary by lines.
Extrude Area about an axis,90 degrees
Quarter of gas cylinder rotated about y axis(90 degrees)
Apply mesh size controls>Preprocessor>Meshing>Size Controls>Smart Size>Basic>Size level> 3
Apply mesh on volumePrerocessor>Meshing>Mesh>Volume>Free
>pick all(all the volume)
Solution Phase
1)Apply BC(constraints)2)Apply 35Mpa on the concerned internal area
Solution>Define loads>apply>Structural>Displacement>On
AreasClick Plane yz>Ux=0
Solution>Define loads>apply>Structural>Displacement>On
AreasClick Plane yx>Uz=0
Solution>Define loads>apply>Structural>Displacement>On Areas
Click Plane xz>Uy=0
Apply pressure on the concerned area
The End