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/ANIM/SHELL/TENS

/ANIM/SHELL/TENS

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/ANIM/SHELL/TENS

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Engine Keyword

/ANIM/SHELL/TENS - Animation of Shell Tensor Results

Description

Generates animation files containing shell tensor data for a specified result.

Format

/ANIM/SHELL/TENS/Restype/Keyword5/Keyword6

Data

Description

Restype

Output tensor:

STRESS - Stress tensor

STRAIN - Strain tensor

EPSDOT - Strain rate tensor

Keyword5

Result type or location:

MEMB - Membrane

BEND - Bending

UPPER - Upper layer

LOWER - Lower layer

N - Layer number N

ALL - All the layers

Keyword6

Result type or location:

NIP - Number of integration points through layer, N (Comment 6)

ALL - All the integration points (NIP) through the layer, N

UPPER - Upper integration point (NIP) of the upper layer, N

LOWER - Lower integration point (NIP)of the lower layer, N

Comments

1.Stress and strain tensor are output in the elemental coordinate system.
2.Strain tensor is output only if Istrain =1 in shell property (/PROP/TYPE1, /PROP/TYPE10, /PROP/TYPE11, /PROP/TYPE16 and /PROP/TYPE17), except for material laws 15, 19 and greater than or equal to 25 (in these cases strain tensor is output irrespective of Istrain flag value).
3.For STRAIN, UPPER gives E1 + (t/2)k and LOWER gives E1 - (t/2)k.

With E1 being the strain, t is the thickness and k is the curvature. For EPSDOT, strain and curvature are replaced by strain rate and curvature rate.

4.The stress tensor output at UPPER/LOWER (and at N) is available when global integration is not used (N>0 defined in property). In the case of using global integration (N=0), then RADIOSS will output the stress at the midplane, even if the stress at UPPER/LOWER is requested.

The stress at UPPER/LOWER is the stress at the upper most / lower most integration point and not an interpolated value based on curvature like the strain.

5.Options /ANIM/SHELL/TENS/STRESS/MEMB and /ANIM/SHELL/TENS/STRESS/BEND are generalized forces (mean values through thickness) per element. For full-integrated element, mean value of 4 Gauss points of the shell surface is calculated. Shell stress can be considered at the center of the element.
6.This option is available only if Keyword5 = N (for each defined layer N allows to compute shell tensor within each integration point NIP of layer N). This option is only available for property set 51 (/PROP/TYPE51 with multiple integration points through each layer).

Nevertheless, Keyword5=ALL combined with Keyword6=ALL is allowed.