A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior

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The book outlines a method for virtual testing of sandwich panel joints, emphasizing its potential to minimize the need for extensive physical testing in lightweight product development. Utilizing the Building Block Approach and Finite Elements Method, it details the creation and validation of sub-models derived from numerous physical tests on sandwich materials. These sub-models are synthesized into comprehensive top-level models, ultimately demonstrating the application of this approach in creating an innovative sandwich panel joint.