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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“Aerospace materials scientists and structural engineers now have a new state-of-the-art software product called StressCheck, which provides efficient and reliable analysis tools for composite bonded aircraft structures. A composites research team from the aeronautics industry, known as the Composites Affordability Initiative (CAI), has just completed an extensive study of current capabilities in the area of failure analysis tools for composite bonded joints. This study led the CAI team to unanimously choose StressCheck as the software tool to replace as well as radically improve existing industry standard software currently used to size bonded joints.”
Air Force Research Laboratory (AFRL)