New scheme for the optimum design of stiffened composite panels with geometric imperfections

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

Volumn 1, Issue , 1999, Pages 588-600

  Elseifi, M A ^a   Gurdal, Z ^a   Nikolaidis, E ^a  

^a VIRGINIA POLYTECHNIC INSTITUTE AND STATE UNIVERSITY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BUCKLING; COMPRESSIVE STRESS; COMPUTER SIMULATION; DEFECTS; FINITE ELEMENT METHOD; GEOMETRY; MATHEMATICAL MODELS; OPTIMIZATION; STIFFNESS; STRUCTURAL PANELS;

COMPOSITE PANELS; GEOMETRIC IMPERFECTIONS; NONLINEAR POSTBUCKLING;

AIRCRAFT PARTS AND EQUIPMENT;

EID: 0032666783     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Article

References (22)