Aeroelastic stability consideration of supersonic flight vehicle using nonlinear aerodynamic response surfaces

Journal of Fluids and Structures

Volumn 25, Issue 6, 2009, Pages 1079-1101

  Fathi Jegarkandi, M ^a   Nobari, A S ^a   Sabzehparvar, M ^a   Haddadpour, H ^b  

^a AMIRKABIR UNIVERSITY OF TECHNOLOGY   (Iran)

^b SHARIF UNIVERSITY OF TECHNOLOGY   (Iran)

Author keywords

Aeroelasticity; Generalized coordinates; Response surface; Simulation code; Stability

Indexed keywords

AEROELASTIC INSTABILITIES; AEROELASTIC STABILITY; AEROELASTICITY; ANALYTICAL MODEL; ANGLE-OF-ATTACK; CFD CODES; FLIGHT VEHICLES; GENERALIZED COORDINATES; GRAM-SCHMIDT; LINEAR STRUCTURAL MODEL; LOCAL VARIATIONS; MODELING FUNCTIONS; MULTIVARIATE FUNCTION; NON-LINEAR AERODYNAMICS; NON-LINEAR DYNAMICS; RESPONSE SURFACE; SIDESLIP ANGLES; SIMULATION CODE; SQUARED ERRORS; SUPERSONIC FLIGHTS;

ELASTIC WAVES; ELASTICITY; FLIGHT DYNAMICS; GAS DYNAMICS; MODEL STRUCTURES; STABILITY; SURFACE PROPERTIES; VEHICLES;

SIMULATORS;

EID: 68749085841     PISSN: 08899746     EISSN: 10958622     Source Type: Journal    
DOI: 10.1016/j.jfluidstructs.2009.04.006     Document Type: Article

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