Some simple solutions for buckling loads of thin and moderately thick cylindrical shells and panels made of laminated composite material

Aerospace Science and Technology

Volumn 1, Issue 1, 1997, Pages 47-63

  Geier, B ^a   Singh, G ^b  

^a Institut für Strukturmechanik   (Germany)

^b INDIAN SPACE RESEARCH ORGANISATION   (India)

Author keywords

Bifurcation; Buckling; Composite materials; Laminates; Panels; Shells

Indexed keywords

EID: 0031492469     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(97)90023-7     Document Type: Article

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