CLT Documentation

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

Laminate Properties

The laminate is defined ply-by-ply using the shared Ply Builder. Each ply is characterized by its material properties, fiber orientation, thickness, and allowable limits.

Ply Properties

For each ply in the stack, the following properties are required:

PropertyUnitsDescription
MaterialLabel for the ply material (informational only)
AngledegreesFiber orientation angle relative to the loading (x) axis
ET1MsiLongitudinal tensile modulus in the fiber (1) direction
EC1MsiLongitudinal compressive modulus in the fiber (1) direction
ET2MsiTransverse tensile modulus in the matrix (2) direction
EC2MsiTransverse compressive modulus in the matrix (2) direction
G12MsiIn-plane shear modulus
ν12Major Poisson's ratio
tinPly thickness
ε₁tμε1-direction tension strain allowable
ε₁cμε1-direction compression strain allowable
ε₂tμε2-direction tension strain allowable
ε₂cμε2-direction compression strain allowable
γ₁₂sμεIn-plane shear strain allowable

CLT carries separate tension and compression moduli (ET1/EC1, ET2/EC2) per ply. Stress allowables are derived from strain allowables using the appropriate directional modulus.

Material Presets

Several built-in material presets are provided for common aerospace composite systems:

  • T300/977-14AC Fabric (70°F) — Balanced woven fabric, commonly used in secondary structure
  • IM7/8552 UD Tape (70°F) — High-performance unidirectional tape for primary structure
  • AS4/3501-6 UD Tape (70°F) — Legacy aerospace unidirectional tape
  • IM7/8552 Plain Weave (70°F) — Balanced plain weave fabric
  • Custom Material — User-defined properties

Preset properties can be edited in-place. Any changes are session-local and do not persist between page reloads.

Ply Stack Operations
  • Quick Add — Adds a ply at 0°, 45°, −45°, or 90° using the currently selected preset’s properties.
  • Bulk Add Plies — Quickly add multiple plies at a specific angle all at once.
  • Custom Ply — Adds a ply at 0° that you can then edit to any angle.
  • Symmetric — Mirrors the current stack to create a symmetric laminate (appends the reverse of the current plies).
  • Repeat — Duplicates the entire current stack and appends it.
  • Clear — Removes all plies from the stack.
  • Move Up/Down — Reorders individual plies within the stack.
  • Delete — Removes an individual ply.

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.

Quick Add Ply Angle
Bulk Add Plies
@
Ply Stack 0 plies
Use the quick-add buttons above to build your layup stack.
Total Thickness:0 in