Computational aeroelastic studies of a generic hypersonic vehicle

Aeronautical Journal

Volumn 113, Issue 1150, 2009, Pages 763-774

  Thuruthimattam, B J ^a   Friedmann, P P ^a   Powell, K G ^a   Bartels, R E ^b  

^a UNIVERSITY OF MICHIGAN   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; COMPUTATION THEORY; HYPERSONIC AERODYNAMICS; HYPERSONIC VEHICLES; PISTONS; VERTICAL STABILIZERS;

AEROELASTIC PROBLEMS; COMPLEX CONFIGURATION; COMPUTATIONAL RESOURCES; DAMPING CHARACTERISTICS; GENERIC HYPERSONIC VEHICLES; THIRD-ORDER PISTON THEORIES; THREE DIMENSIONAL EFFECT; THREE-DIMENSIONAL FLOW;

AEROELASTICITY;

EID: 77952246362     PISSN: 00019240     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0001924000003420     Document Type: Article

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