Response surface based laminate stacking sequence optimization under stability constraints

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 3, Issue , 1997, Pages 2381-2389

  Gangadharan, S N ^a   Nagendra, S ^a   Fiocca, Y ^a  

^a EMBRY RIDDLE AERONAUTICAL UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY CONDITIONS; BUCKLING; LAMINATED COMPOSITES; OPTIMIZATION; PLATES (STRUCTURAL COMPONENTS); POLYNOMIALS; STRUCTURAL DESIGN;

CONTINUOUS RESPONSE SURFACE REFINEMENT METHOD; LAMINATE STACKING SEQUENCE; STABILITY CONSTRAINTS;

COMPOSITE STRUCTURES;

EID: 0030643665     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (14)