Maximum Strain and Maximum Stress Criteria

These criteria do not consider any interaction between different stress (strain components).

The failure occurs if one of the following conditions are satisfied:
  • σ1XTσ1XT or σ1XCσ1XC
  • σ2YTσ2YT or σ2YCσ2YC
  • τ12Sτ12S
Being σ1 σ2σ1 σ2 and τ12τ12 the in-plane normal stress components and the in-plane shear stress one respectively and where:
  • Xt,XcXt,Xc are the maximum allowable stresses in the 1-direction in tension and compression,
  • Yt,YcYt,Yc are the maximum allowable stresses in the 2-direction in tension and compression,
  • SS is the allowable in-plane shear stress

Relevant failure index is evaluated as per the following equation:

Findex=max[σ1X,σ2Y,τ12S]Findex=max[σ1X,σ2Y,τ12S]

being X=XTX=XT or X=XCX=XC if σ10σ10  or σ1<0σ1<0 and the same for YY .

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).