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Published in:
2020 | OriginalPaper | Chapter
Summary and outlook
Author : Ralf Seemann
Published in: A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior
Publisher: Springer Berlin Heidelberg
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The determination of the mechanical properties by means of physical testing is a major cost driver in the development process of lightweight products. The implementation of virtual tests based on FE-simulations can be a significant contributor to reducing the development cost. However, composite sandwich structures are characterized by a complicated failure behavior, making reliable predictions via FE-simulations challenging. The present work addresses this problem by establishing a virtual testing approach for sandwich structures.