Abstract
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.
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Seemann, R. (2020). Summary and outlook. In: A Virtual Testing Approach for Honeycomb Sandwich Panel Joints in Aircraft Interior. Produktentwicklung und Konstruktionstechnik, vol 16. Springer Vieweg, Berlin, Heidelberg. https://doi.org/10.1007/978-3-662-60276-8_9
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DOI: https://doi.org/10.1007/978-3-662-60276-8_9
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Publisher Name: Springer Vieweg, Berlin, Heidelberg
Print ISBN: 978-3-662-60275-1
Online ISBN: 978-3-662-60276-8
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