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Strength of sandwich beams with mid-plane debondings in the core

✍ Scribed by Dan Zenkert

Publisher
Elsevier Science
Year
1990
Tongue
English
Weight
885 KB
Volume
15
Category
Article
ISSN
0263-8223

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The post failure behaviour of sandwich panels loaded in in-plane compression is studied by considering the structural response of such panels with symmetrically located edge debonds. A parametric finite element model is used to determine the influence of different material and geometrical properties

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A systematic experimental study to determine the effect of curvatures and debond on the flexural stiffness and strength of composite sandwich beam structures made from fiber-glass/epoxy laminate skins and polyurethane foam core has been carried out. Flat and curved sandwich beams (with 15Β°, 30Β°, 45Β°