Efficient and realistic simulation of composite bolted joints is absolutely necessary in fully realizing the
This whitepaper will present a computationally efficient method for modeling thick composite bolted joints to aid in aircraft structures analysis.
See how the modeling strategy identifies the joint parameters to accurately capture load distributions in composite joints. Also learn how the MultiContinuum Theory (MCT) damage model is utilized as part of the modeling strategy to extract separate failure predictions for the fibers and epoxy matrices throughout the composite joints.
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"...I am impressed at your company's willingness to quickly react to and address our issues. Your good work in your product is already being used to help us design the first commercial man carrying spaceship."
Dan Kreigh, Lead Structural Analysts, Scaled Composites
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