These criteria do not consider any interaction between different stress (strain
components).
The failure occurs if one of the following conditions are satisfied:
-
or
-
or
-
Being
and
the in-plane normal stress components and the in-plane shear
stress one respectively and where:
-
are the maximum allowable stresses in the 1-direction in
tension and compression,
-
are the maximum allowable stresses in the 2-direction in
tension and compression,
-
is the allowable in-plane shear stress
Relevant failure index is evaluated as per the following equation:
being
or
if
or
and the same for
.
The approach for maximum strain criterion is the same as per the maximum stress on, but
with the corresponding strains in the condition for failure to be taken into account.
Syntax
MaxStrainFT(tensor,xt,xc,yt,yc,s,sets,plies,elems,parts,props,pool_name,layer_index,opt_str)
Arguments
- tensor
- Stress table
- xt
- Allowable tensile stress/strain in ply material direction 1
- xc
- Allowable compressive stress/strain in ply material direction 1
- yt
- Allowable tensile stress/strain in ply material direction 2
- yc
- Allowable compressive stress/strain in ply material direction 2
- s
- Allowable in-plane shear stress/strain
- sets
- Set table (D=NULL)
- plies
- Ply table (D=NULL)
- elems
- Element table (D)
- parts
- Part table (D)
- props
- Property table (D)
- pool_name
- Pool name (D=@current_pool)
- layer_index
- Layer index (D=@current_slice_index)
- opt_str
- This is an optional argument, which can passed if needed (D=option).