Development of an Euler/Navier-stokes aeroelastic method for three-dimensional vehicles with multiple flexible surfaces

37th AIAA/ASME/ASCE/AHS/ASC Structure, Structural Dynamics and Materials Conference

Volumn , Issue , 1996, Pages 1733-1746

  Smith, Marilyn I ^a   Schuster, David M ^b   Huttsell, Larry ^c   Button, Brad ^d  

^a GEORGIA TECH RESEARCH INSTITUTE   (United States)

^b Lockheed Martin Engineering and Science Services   (United States)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d AIR FORCE INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC CONFIGURATIONS; AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; DYNAMICS; FIGHTER AIRCRAFT; STRUCTURAL ANALYSIS; STRUCTURAL DYNAMICS; VERTICAL STABILIZERS; FLEXIBLE STRUCTURES; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; PERFORMANCE; SHELLS (STRUCTURES); THREE DIMENSIONAL; UNSTEADY FLOW;

AEROELASTIC ANALYSIS; COMPUTATIONAL FLUID DYNAMICS METHODS; DISSIPATION MODELS; FLEXIBLE SURFACES; FLIGHT CONDITIONS; LINEAR STRUCTURAL MODEL; SHELL STRUCTURE; UNSTEADY AERODYNAMICS;

AEROELASTICITY; AERODYNAMICS;

ENHANCED DISSIPATION MODELS; EULER/NAVIER-STOKES THREE DIMENSIONAL AEROELASTIC; GRID GENERATION; MULTIPLE FLEXIBLE SURFACES; REAL GAS CAPABILITY;

EID: 0029700435     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1996-1513     Document Type: Conference Paper

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