Implementation of strength-based failure criteria in the lamination parameter design space

AIAA Journal

Volumn 46, Issue 7, 2008, Pages 1826-1834

  Ijsselmuiden, Samuel T ^a,b   Abdalla, Mostafa M ^a,b   Gürdal, Zafer ^a,b,c  

^a DELFT UNIVERSITY OF TECHNOLOGY   (Netherlands)

^b Aerospace Structures ^*

^c Aerospace Structures Chair   (Netherlands)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREE OF CORRELATIONS; DESIGN OPTIMIZATION (DO); DESIGN SPACES; DESIGN VARIABLES; FAILURE CRITERION; FAILURE ENVELOPES; FIBER ANGLES; FIBER ORIENTATION (ANGLE); FREE REGION; LAMINATE STACKING SEQUENCE; LAMINATION PARAMETERS; OBJECTIVE FUNCTION (OF); OPTIMIZATION PROCESSES; PARAMETER DESIGNS; PARAMETER SPACES; STACKING SEQUENCES; STRENGTH (IGC: D5/D6); STRENGTH CRITERION; TSAI-WU FAILURE CRITERION;

COMPOSITE STRUCTURES; CONSTRAINED OPTIMIZATION; FIBER OPTICS; LAMINATES; OPTIMIZATION; STIFFNESS; STRUCTURAL OPTIMIZATION; STRUCTURE (COMPOSITION);

LAMINATING;

EID: 47749116814     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.35565     Document Type: Conference Paper

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