StressCheck Tutorial: Laminated Composite Repair Patch Part II – Materials, BC’s & Results
Abstract: Modeling a laminated composite repair patch. Rectangular plate with circular cutout bonded with a rectangular laminated composite repair patch.
Part II: material definition and assignment via automatic lamination, application of boundary conditions, solution by p-extension and live dynamic results.
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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)