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Published in:
2020 | OriginalPaper | Chapter
State of the art
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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Sandwich structures are based on the principle of separating two thin and stiff faces by a thick, mechanically weak lightweight core. Load transfer between these three components is achieved by adhesive bonding (Figure 2). This arrangement functions like an Ibeam, where as much material as possible is placed farthest away from the neutral axis, thus providing excellent weight specific bending stiffness and strength.