Zigzag sublaminate model for nonlinear analysis of laminated panels

Journal of Aerospace Engineering

Volumn 13, Issue 3, 2000, Pages 100-109

  Eby, David ^a   Averill, Ronald C ^b  

^a ACD Associates   (United States)

^b Michigan State University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BENDING (DEFORMATION); COMPOSITE STRUCTURES; DEGREES OF FREEDOM (MECHANICS); DYNAMIC RESPONSE; FINITE ELEMENT METHOD; KINEMATICS; LAMINATED COMPOSITES; MATHEMATICAL MODELS; PLATES (STRUCTURAL COMPONENTS); STRUCTURAL ANALYSIS; STRUCTURAL PANELS; TOPOLOGY;

LAMINATED PANELS; STRUCTURAL RESPONSE;

AIRFRAMES;

EID: 0034230435     PISSN: 08931321     EISSN: None     Source Type: Journal    
DOI: 10.1061/(ASCE)0893-1321(2000)13:3(100)     Document Type: Article

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