AIAA-2004-2055 Optimum Design of Filament-Wound Laminated Conical Shells for Buckling Using a Response Surface Methodology
45TH, Structures, structural dynamics, and materials conference:; 45th AIAA/ASME/ASCE/AHS/ASC 12th AIAA/ASME/AHS adaptive structures conference: 6th AIAA non-deterministic approaches forum: 5th AIAA gossamer spacecraft forum ; 2004 ; Palm Springs, Calif
01.01.2004
8 pages
Held in conjunction with 12th AIAA/ASME/AHS adaptive structures conference, 6th AIAA non-deterministic approaches forum and 5th AIAA gossamer spacecraft forum
Aufsatz (Konferenz)
Englisch
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Buckling of Filament Wound Composite Conical Shells Under Axial Compression
British Library Conference Proceedings | 1998
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