1) Build your material stack
Select orthotropic plies or add custom materials with E₁/E₂, G₁₂, ν₁₂, thickness, and density. Capture thermal coefficients (α₁/α₂) to drive expansion analysis.
Simple orthotropic material database and laminate designer complete with analysis tools employing different laminate models
Choose materials from the database or contribute your own
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Design your laminate with symmetry and repetition controls
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Click "Add Layer" or select a stacking sequence
No custom sequences saved yet
Select analysis tools and configure geometry and loading conditions
Configure tool settings and run analysis
No tools selected. Please go back to step 3 to select tools.
Getting started
Move from material selection to laminate validation with steps aligned to Classical Laminate Theory (CLT), thermal expansion checks, and failure criteria verification.
Select orthotropic plies or add custom materials with E₁/E₂, G₁₂, ν₁₂, thickness, and density. Capture thermal coefficients (α₁/α₂) to drive expansion analysis.
Use repetition counts, before/after symmetry controls, and preset sequences (quasi-isotropic, cross-ply) to speed up stacking sequence creation.
Attach stiffness, displacement, thermal, and failure tools, then set coupon dimensions and load cases to mirror your test setup.
Inspect ABD matrices, mid-plane strains/curvatures, thermal responses, and Tsai-Hill/Tsai-Wu margins to validate the laminate before fabrication.
FAQ
Targeted guidance for engineers, researchers, and students working on composite laminate analysis and validation.
The platform assembles ply stiffness contributions into ABD matrices, computes mid-plane strains and curvatures, and surfaces laminate-level responses so you can verify stiffness, coupling, and thermal effects.
Yes. Provide α₁ and α₂ for each ply, select the thermal analysis tool, and the solver integrates these coefficients to show laminate thermal expansion and temperature-dependent behavior.
The analysis tools include Tsai-Hill and Tsai-Wu options with inputs for Xₜ/Xc, Yₜ/Yc, and S to compute safety margins for each ply.
Save custom sequences in the designer and reapply them across projects; presets are available for common layups like quasi-isotropic and cross-ply.
The web application is free to use for all visitors. You can create an account to store custom materials, layups, and tool configurations.
Trying to be a comprehensive and straightforward web-based laminate calculator for engineers, researchers, and students. Interactively design your laminate and perform analysis using different tools.
Complete Classical Laminate Theory calculations with ABD matrix computations and laminate stiffness constants.
Advanced thermal expansion analysis with through-thickness stress calculations and thermal cycling effects.
Interactive stacking sequence designer with symmetry controls and ply orientation optimization.
Comprehensive failure criteria evaluation including Tsai-Wu, Hashin, and maximum stress criteria.
Advanced microcrack detection and propagation analysis for composite materials under various loading conditions.
Fracture toughness evaluation including mode I, mode II, and mixed-mode fracture analysis.