Aero-thermo-mechanical characteristics of imperfect shape memory alloy hybrid composite panels

Journal of Sound and Vibration

Volumn 325, Issue 3, 2009, Pages 583-596

  Ibrahim, Hesham Hamed ^a,b   Yoo, Hong Hee ^a   Lee, Kwan Soo ^a  

^a Hanyang University   (South Korea)

^b National Authority for Remote Sensing and Space Sciences   (Egypt)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC PRESSURE; COMBINED EFFECT; COMPOSITE PANELS; CURVED PLATES; EIGENVALUE PROBLEM; EMBEDDINGS; EQUILIBRIUM POSITIONS; FIRST-ORDER; FREE VIBRATION CHARACTERISTIC; FREE VIBRATION FREQUENCY; GEOMETRIC IMPERFECTION; GOVERNING EQUATIONS; LARGE DEFLECTION; MATERIAL PROPERTY; NEWTON-RAPHSON ITERATION METHOD; NON-LINEAR FINITE ELEMENT MODEL; NONLINEAR STRAIN; PISTON THEORY; PRINCIPLE OF VIRTUAL WORK; QUASI-STEADY; SHAPE MEMORY ALLOY FIBERS; SHAPE MEMORY ALLOY HYBRID COMPOSITES; STATIC AERODYNAMIC LOADS; TEMPERATURE DEPENDENCE; TEMPERATURE RISE; THERMAL DEFLECTIONS; THERMO-MECHANICAL CHARACTERISTICS; VIBRATION BEHAVIOR; VON KARMAN;

AERODYNAMIC LOADS; AERODYNAMICS; ALLOYS; DEFLECTION (STRUCTURES); EIGENVALUES AND EIGENFUNCTIONS; PLATES (STRUCTURAL COMPONENTS); TEMPERATURE DISTRIBUTION; THERMOANALYSIS;

NONLINEAR EQUATIONS;

EID: 67349215788     PISSN: 0022460X     EISSN: 10958568     Source Type: Journal    
DOI: 10.1016/j.jsv.2009.03.027     Document Type: Article

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