Lamination parameters applied to reliability-based in-plane strength design of composites

AIAA Journal

Volumn 41, Issue 11, 2003, Pages 2200-2207

  Kogiso, Nozomu ^a,b   Nakagawa, Shuuya ^a,b   Murotsu, Yoshisada ^a  

^a Osaka Prefecture University   (Japan)

^b Osaka Prefectural Coll of Technol ^*  (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PARTS AND EQUIPMENT; COMPUTER AIDED DESIGN; FAILURE ANALYSIS; LAMINATED COMPOSITES; OPTIMIZATION; RELIABILITY;

FIRST PLY FAILURE CRITERIA; RELIABILITY BASED OPTIMIZATION DESIGN;

AIRCRAFT MATERIALS;

EID: 0346215913     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.6812     Document Type: Article

References (14)

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