Nonlinear dynamic behavior of simply supported laminated composite plates subjected to blast load

Journal of Sound and Vibration

Volumn 317, Issue 3-5, 2008, Pages 883-897

  Kazanci, Zafer ^a   Mecitoǧlu, Zahit ^b  

^a TURKISH AIR FORCE ACADEMY   (Turkey)

^b ISTANBUL TECHNICAL UNIVERSITY   (Turkey)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC LOADS; CONTROL NONLINEARITIES; CONTROL THEORY; DIFFERENCE EQUATIONS; DIFFERENTIAL EQUATIONS; DIFFERENTIATION (CALCULUS); DYNAMIC LOADS; DYNAMIC RESPONSE; EXPLOSIVES; FINITE DIFFERENCE METHOD; FINITE ELEMENT METHOD; GALERKIN METHODS; LAMINATED COMPOSITES; LAMINATING; MILITARY DATA PROCESSING; NUMERICAL ANALYSIS; PLATES (STRUCTURAL COMPONENTS);

APPROXIMATE SOLUTIONS; APPROXIMATION FUNCTIONS; BLAST LOADS; COUPLED NONLINEAR EQUATIONS; DYNAMIC EQUATIONS; FINITE DIFFERENCE (FD); FINITE ELEMENT (FE); GALERKIN; GEOMETRIC NON LINEARITIES; LAMINATED COMPOSITE PLATES; LARGE DEFLECTION THEORY; NON LINEAR DIFFERENTIAL EQUATIONS; NONLINEAR DYNAMIC BEHAVIORS; NONLINEAR DYNAMIC RESPONSE; SIMPLY SUPPORTED; SPACE DOMAINS; STATIC DEFORMATIONS; THIN PLATES; TIME DOMAIN (OCT); VIRTUAL WORK PRINCIPLE (VWP);

NONLINEAR EQUATIONS;

EID: 48349085757     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2008.03.033     Document Type: Article

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