CLT Documentation

Complete reference for the Classical Lamination Theory analysis tool — laminate setup, applied loads, stiffness matrices, failure criteria, and theoretical background.

Applied Loads

CLT evaluates laminate response to applied force resultants (N) and moment resultants (M). All loads are specified as running loads (force per unit width) or moments (moment per unit width).

Force & Moment Resultants
ParameterUnitsDescription
Nxlb/inIn-plane running load in the x-direction
Nylb/inIn-plane running load in the y-direction
Nxylb/inIn-plane shear running load
Mxin·lb/inBending moment per unit width about the y-axis
Myin·lb/inBending moment per unit width about the x-axis
Mxyin·lb/inTwisting moment per unit width
Load Conventions

Two load sign conventions are supported to match different workflow expectations:

  • CLT (Default) — Standard CLT convention where a positive Mx produces tension on the bottom surface (positive z) and compression on the top surface (negative z).
  • NASTRAN — NASTRAN convention where the sign of Mx, My, and Mxy is reversed relative to CLT convention. Switching conventions automatically negates the moment values.
Note: Switching conventions flips the sign of all three moment components (Mx, My, Mxy) in-place. The force resultants (Nx, Ny, Nxy) are unaffected.

Shared Laminate Builder

Laminate Properties

Input Allowables Format

Toggle between Strain (με) and Stress (ksi). Values in the stack and limits will convert on-the-fly.

NameET1 (Msi)EC1 (Msi)ET2 (Msi)EC2 (Msi)G12 (Msi)ν12t (in)σ₁t (ksi)σ₁c (ksi)σ₂t (ksi)σ₂c (ksi)σ₁₂s (ksi)r_c Tens (in)r_c Comp (in)K_br TensK_br Comp
Save as Custom Preset

Save the current material properties under a name so you can reuse them without re-entering values.

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