Supersonic flutter prediction of functionally graded conical shells

Composite Structures

Volumn 92, Issue 2, 2010, Pages 377-386

  Mahmoudkhani, S ^a   Haddadpour, H ^a   Navazi, H M ^a  

^a SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

Conical shell; Functionally graded materials; Panel flutter; Supersonic; Thermal effects

Indexed keywords

AERODYNAMIC LOADING; AEROELASTIC STABILITY; AIR FLOW; CONE ANGLE; CONICAL SHELL; EQUILIBRIUM EQUATION; FIRST-ORDER; FLUTTER BOUNDARIES; FUNCTIONALLY GRADED; INITIAL STRESS; KINEMATIC NONLINEARITY; LINEAR EQUILIBRIUM; PANEL FLUTTER; PISTON THEORY; POWER SERIES METHOD; POWER-LAW FUNCTIONS; SHELL THEORY; SIMPLE RULES; SIMPLY SUPPORTED; STABILITY ANALYSIS; SUPERSONIC; SUPERSONIC FLUTTER; TEMPERATURE-DEPENDENT PROPERTIES; THERMAL ANALYSIS; THERMAL LOADINGS; THERMOELASTIC ANALYSIS; TRUNCATED CONICAL SHELL; VOLUME FRACTION INDEX; VON KARMAN;

CONTROL NONLINEARITIES; CRACK INITIATION; EQUATIONS OF MOTION; FLUTTER (AERODYNAMICS); GALERKIN METHODS; GAS DYNAMICS; LINEARIZATION; LOADING; MECHANICS; NONLINEAR EQUATIONS; OPEN CHANNEL FLOW; PLATES (STRUCTURAL COMPONENTS); SHELLS (STRUCTURES); THERMAL EFFECTS; THERMOANALYSIS; TITRATION; TRAJECTORIES;

FUNCTIONALLY GRADED MATERIALS;

AERODYNAMICS; AIRFLOW; CONDUCTIVITY; PREDICTION; STABILITY; STRUCTURAL ANALYSIS; TEMPERATURE; THERMAL ANALYSIS;

EID: 70349843061     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2009.08.018     Document Type: Article

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