Aeroelastic and aerothermoelastic behavior in hypersonic flow

AIAA Journal

Volumn 46, Issue 10, 2008, Pages 2591-2610

  McNamara, Jack J ^a,c,d   Friedmann, Peretz P ^a,c   Powell, Kenneth G ^a,c   Thuruthimattam, Biju J ^a,c,e   Bartels, Robert E ^b,f  

^a UNIVERSITY OF MICHIGAN   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

^c Department of Aerospace Engineering ^*

^d The Ohio State University   (United States)

^e BlackRock Inc   (United States)

^f Aeroelasticity Branch

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC MODELS; AEROELASTIC ANALYSES; AEROELASTIC BEHAVIORS; AEROTHERMOELASTIC BEHAVIORS; AEROTHERMOELASTICITY; COMPUTATIONAL AEROELASTICITIES; COMPUTATIONAL STUDIES; CONTROL SURFACES; FLUTTER BOUNDARIES; FLUTTER MARGINS; GRID RESOLUTIONS; HIGH ALTITUDES; HYPERSONIC FLIGHTS; HYPERSONIC VEHICLES; PISTON THEORIES; SIGNIFICANT REDUCTIONS; SOLUTION PROCEDURES; STRUCTURAL VARIATIONS; THERMAL BUCKLING; TUNNEL MODELS;

AERODYNAMIC HEATING; AIR; AIRCRAFT INSTRUMENTS; ASPECT RATIO; BUCKLING; COMPRESSIBILITY; DYNAMICS; FLUTTER (AERODYNAMICS); GAS DYNAMICS; HEATING; HYPERSONIC AERODYNAMICS; HYPERSONIC FLOW; MACH NUMBER; SENSITIVITY ANALYSIS; THERMODYNAMICS; THREE DIMENSIONAL; TRAJECTORIES; TWO PHASE FLOW; WIND TUNNELS; WINGS;

AERODYNAMICS;

EID: 54549087792     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.36711     Document Type: Article

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