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¦
Delamination from localized instabilities in compression sandwich panels
β Scribed by M.Ahmer Wadee; A. Blackmore
- Book ID
- 108358617
- Publisher
- Elsevier Science
- Year
- 2001
- Tongue
- English
- Weight
- 454 KB
- Volume
- 49
- Category
- Article
- ISSN
- 0022-5096
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