The nonlinear dynamic behaviour of tapered laminated plates subjected to blast loading

Shock and Vibration

Volumn 19, Issue 6, 2012, Pages 1235-1255

  Susler, Sedat ^a   Turkmen, Halit S ^a   Kazanci, Zafer ^b  

^a ISTANBUL TECHNICAL UNIVERSITY   (Turkey)

^b TURKISH AIR FORCE ACADEMY   (Turkey)

Author keywords

blast loading; finite element method; laminated composite plate; large deflection; nonlinear analysis; Tapered plate

Indexed keywords

EQUATIONS OF MOTION; FINITE ELEMENT METHOD; GALERKIN METHODS; LAMINATED COMPOSITES; LAMINATING; NONLINEAR ANALYSIS;

AIR BLAST; ALGEBRAIC DIFFERENTIAL EQUATION; APPROXIMATE SOLUTION; BLAST LOADING; DYNAMIC BEHAVIOURS; FIBER ORIENTATION ANGLE; FINITE DIFFERENCE APPROXIMATIONS; FINITE ELEMENT SOFTWARE; GEOMETRIC NON-LINEARITY; GEOMETRICALLY NONLINEAR; IN-PLANE STIFFNESS; LAMINATED COMPOSITE PLATES; LAMINATED PLATE; LARGE DEFLECTION; SIMPLY SUPPORTED; SPACE DOMAIN; STACKING SEQUENCE; TAPER RATIOS; TAPERED PLATE; TIME DOMAIN; VIRTUAL WORK PRINCIPLE;

DYNAMIC RESPONSE;

EID: 84872453242     PISSN: 10709622     EISSN: None     Source Type: Journal    
DOI: 10.3233/SAV-2012-0667     Document Type: Conference Paper

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