The Composites Affordability Initiative (CAI) unanimously selected ESRD’s composites functionality to “replace as well as radically improve existing industry software currently used for bonded joints.” In time, the improvements extended to fastened laminated composite and metallic-laminated joints, reinforced composite structures, multi-scale analysis and more.
Composites Applications
Our implementation is unique in the FEA industry for focusing on the detailed analysis needs of composite designers and engineers, including 3D ply-by-ply modeling and failure analysis.
Schedule a Composites Demo
Would you like a no-cost demonstration of our composites engineering application solutions? Complete our Request an Engineering Application Demo form and we will get back to you shortly.
Composites Application Focus
The following are typical composites analysis applications which are routinely performed in StressCheck Professional:
Linear Elasticity Solver
Composites Module
Non-Linear Solver
Margin Check Solver
Linear Elasticity Solver
Composites Module
Non-Linear Solver
Margin Check Solver
Heat Transfer Solver
Linear Elasticity Solver
Composites Module
Heat Transfer Solver
Would you like to schedule a Composites Analysis Demo?
Would you like to learn more about our features and solutions for laminated composites analysis applications? Schedule a Composites Analysis demo with us by completing the below form and we’ll contact you as soon as possible. Thank you!
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Testimonials
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“A screening of existent commercial and non-commercial tools was carried out in respect to their fracture mechanics capabilities, their design abilities, implementation as well as their complexity. Although, there are many software possibilities, only those within the reach of the author were evaluated. This resulted in the selection of the commercial tool StressCheck. The assessment of crack propagation on compact tension and two stringer specimens governed by the Paris and Forman regimes was satisfactory compared with experimental results using the material data from simple standard specimens.”
Lloren Llopart Prieto (EADS)
Doctoral Thesis, "Modelling and analysis of crack turning on aeronautical structures"