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ABAQUS Tutorial: Continuum vs. solid vs. 2-D shell elements for
buckling analysis of composite shells
Presentation · September 2020
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Ronald Heinz Norbert Wagner
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Material parameter
Laminate Stacking (skin)
Elasticity modulus 𝐸11 - [𝑁/𝑚𝑚2 ]
Elasticity modulus 𝐸22 - [𝑁/𝑚𝑚2 ]
Poisson’s ratio ν12
Shear modulus - 𝐺12 - [𝑁/𝑚𝑚2 ]
Shear modulus - 𝐺23 - [𝑁/𝑚𝑚2 ]
Geometry parameter
Large radius R - [mm]
Length L - [mm]
Ply thickness tp - [mm]
Effective Thickness teff - [mm]
R/teff
L/R
Cylinder Z36
[34,-34,0,0,53,-53]
152400
8800
0.31
4900
3230
400
800
0.125
0.726
550.47
2.0
400.750
400.625
400.500
400.375
400.250
400.125
400
C3D8R
SC8R
S4R
Exp. - Z36
C3D20
Axial Force F [kN]
120
100
80
60
40
20
0
0
0.05
0.1
0.15
0.2
0.25
0.3
0.35
0.4
0.45
0.5
0.55
Axial Displacement u [mm]
0.6
0.65
0.7
0.75
ABAQUS Tutorial: Continuum vs. solid vs. 2-D shell elements for buckling analysis of composite cylinders
In this video,
https://youtu.be/ajZ1cOU4708
I will compare different modelling methods for composite shells!
Conventional shell elements (2D): 0:44
Continuum shell element (2.5D): 6:32
Solid element (3D): 15:19
Important settings for C3D20 elements (quadratic shape functions and full integration): 29:52
Result overview: 31:00
Comparison of buckling loads: 32:30
#buckling #abaqus #abaqustutorial #hnrwagner
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