Reynolds-averaged Navier-Stokes solutions for the CAWAPI F-16XL using different hybrids grids

Journal of Aircraft

Volumn 46, Issue 2, 2009, Pages 409-422

  Fritz, Willy ^a,e   Davis, M Bruce ^b,f   Karman Jr , Steve L ^c,g   Michal, Todd ^d  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b LOCKHEED MARTIN   (United States)

^c UNIVERSITY OF TENNESSEE AT CHATTANOOGA   (United States)

^d BOEING COMPANY   (United States)

^e Aerodynamics and Methods   (Germany)

^f Aerodynamics and Computational Fluid Dynamics ^*

^g Graduate School of Computational Engineering   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; DELTA WING AIRCRAFT; FLIGHT SIMULATORS; NAVIER STOKES EQUATIONS; RESEARCH AIRCRAFT;

BOEING PHANTOM WORKS; CRANKED-ARROW WING; FULL-SCALE MODELING; LOCKHEED MARTIN AERONAUTICS COMPANIES; REYNOLDS - AVERAGED NAVIER-STOKES; UNIVERSITY OF TENNESSEE; UNSTRUCTURED GRID; VISCOUS SIMULATIONS;

SUPERSONIC AIRCRAFT;

EID: 63349105166     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.35106     Document Type: Article

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