Beam Failures

The Beam config has two subtypes: Beam_member and Beam_shell. The first is made of 1D elements while the second points to freebody sections. Both configs come with their flavor of the same actual methods:
  1. Stringer Axial Stress
  2. Stringer compressive buckling

The Stinger Axial Stress is a simple method which calculates the Compressive/Tensile margin of safety as:

MS= [(Compressive Stress limit)*(section Area)/(Axial Force)] -1; (resp. Tensile Stress limit)

In the case of freebody sections, Axial Force is mapped to the freebody resultant Fx.

The compressive buckling method evaluates MS=Fcc/σx1 with:
  • σx : average axial stress as (Axial Force)/(Section’s area)
  • Fcc=Fcy*(1.272(L'/ρ)/π*E/Fcy)
  • Fcy : material compressive stress limit
  • L'=(structuralpropertyLength)/K_constraint
    • K_constraint = “constraint coefficient” on structural property. Def=0.0699
  • ρ : beam section’s radius of gyration
  • E: material young’s modulus