Feddal et al., 2021 - Google Patents
Delamination buckling of a laminated composite shell panel using cohesive zone modellingFeddal et al., 2021
View HTML- Document ID
- 3732521478056085097
- Author
- Feddal I
- Khamlichi A
- Publication year
- Publication venue
- International Review of Applied Sciences and Engineering
External Links
Snippet
Laminated composite shell panels take part in several engineering structures. Due to their complex nature, failure modes in composites are highly dependent on the geometry, direction of loading and orientation of the fibers. However, the design of composite parts is …
- 230000032798 delamination 0 title abstract description 135
Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
- B64C1/06—Frames; Stringers; Longerons; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
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