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
β¦ LIBER β¦
Strength of composite sandwich panels containing debonds
β Scribed by W.C. Kim; T.C. Miller; C.K.H. Dharan
- Book ID
- 107773532
- Publisher
- Elsevier Science
- Year
- 1993
- Tongue
- English
- Weight
- 947 KB
- Volume
- 30
- Category
- Article
- ISSN
- 0020-7683
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