Coexisting thermal postbuckling of composite plates with initial imperfections using finite element modal method

37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference

Volumn , Issue , 1996, Pages 1355-1362

  Shi, Yucheng ^a   Meit, Chuh ^a  

^a Old Dominion University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

NONLINEAR EQUATIONS; PLATES (STRUCTURAL COMPONENTS); POTENTIAL ENERGY; STRUCTURAL DYNAMICS; BUCKLING; COMPOSITE STRUCTURES; CONVERGENCE OF NUMERICAL METHODS; DEFECTS; DEFLECTION (STRUCTURES); FINITE ELEMENT METHOD; LAMINATED COMPOSITES; MODAL ANALYSIS; PRESSURE EFFECTS; THERMAL EFFECTS; THERMAL LOAD;

FINITE ELEMENT FORMULATIONS; FINITE ELEMENT MODAL METHOD; INITIATION TEMPERATURE; NONLINEAR MODAL EQUATION; POSTBUCKLING DEFLECTION; THERMAL POST-BUCKLING; THIN COMPOSITE PLATES; TOTAL POTENTIAL ENERGY;

FINITE ELEMENT METHOD; PLATES (STRUCTURAL COMPONENTS);

ANTISYMMETRICAL ANGLE PLY LAMINATE; COMPOSITE PLATES; FINITE ELEMENT MODAL METHODS; INITIAL IMPERFECTIONS; NONLINEAR MODAL EQUATIONS; POSTBUCKLING DEFLECTION SHAPE CHANGE; THERMAL POSTBUCKLING;

EID: 0029710730     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1467     Document Type: Conference Paper

References (12)

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