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Constitutive law for loading (thin) 3D shell elements.
This law is used for mechanical analysis of shells, loaded by uniform pressure and shear, normal and tangential to the mid-line $\xi$ at any moment, or in the global axes.
Loading can be driven either by force multiplicator (MULTF) or displacement multiplicator (MULTD).
Prepro: LLOACQ.F
Lagamine: CLCOQ4.F
Plane stress state | NO |
Plane strain state | NO |
Axisymmetric state | NO |
3D state | YES |
Generalized plane state | NO |
Line 1 (2I5, 60A1) | |
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IL | Law number |
ITYPE | 99 |
COMMENT | Any comment (up to 60 characters) that will be reproduced on the output listing |
Line 1 (I5) | |
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IDIRC | Index of the loading direction |
= 0 : Local direction | |
= 1 : Global direction |
Line 1 (3G10.0) | |
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PRESSF | Pressure $p_o$ (which will be multiplied by MULTF) |
TAURF | Shear $\tau_r$ (which will be multiplied by MULTF) |
TAUSF | Shear $\tau_s$ (which will be multiplied by MULTF) |
Line 1 (3G10.0) | |
PRESS | Pressure $p_o$ (which will be multiplied by MULTD) |
TAURD | Shear $\tau_r$ (which will be multiplied by MULTD) |
TAUSD | Shear $\tau_s$ (which will be multiplied by MULTD) |
3
SIG(1) | = p : Pressure (= $p_o$ * MULT) |
> 0 according with local coordinates of shell | |
SIG(2) | = $\tau$ : Shear (= $\tau_r$ * MULT) |
> 0 according with local coordinates of shell | |
SIG(3) | = $\tau$ : Shear (= $\tau_s$ * MULT) |
> 0 according with local coordinates of shell |
1
Q(1) | Without any meaning |