Standard unstructured grid solutions for cranked arrow wing aerodynamics project international F-16XL

Journal of Aircraft

Volumn 46, Issue 2, 2009, Pages 385-408

  Görtz, Stefan ^a,f   Jirasek A ^b,d   Morton, Scott A ^c,g   McDaniel, David R ^d,g   Cummings, Russell M ^d,g   Laman, John E ^e,h   Abdol Hamid, Khaled S ^e,i  

^a ROYAL INSTITUTE OF TECHNOLOGY   (Sweden)

^b SWEDISH DEFENCE RESEARCH AGENCY   (Sweden)

^c AIR FORCE RESEARCH LABORATORY   (United States)

^d UNITED STATES AIR FORCE ACADEMY   (United States)

^e NASA LANGLEY RESEARCH CENTER   (United States)

^f GERMAN AEROSPACE CENTER DLR   (Germany)

^g Department of Aeronautics ^*

^h NASA Langley Distinguished Research Associate

ⁱ Distinguished Research Associate   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ATMOSPHERIC THERMODYNAMICS; BOUNDARY LAYER FLOW; BOUNDARY LAYERS; COMPUTATIONAL FLUID DYNAMICS; DELTA WING AIRCRAFT; FLIGHT SIMULATORS; FLOW SEPARATION; FLOW SIMULATION; FORECASTING; NAVIER STOKES EQUATIONS; PLANFORMS; RESEARCH AIRCRAFT; TURBULENCE MODELS; TURBULENT FLOW; VISCOUS FLOW; WINGS;

BOUNDARY LAYER VELOCITY; COMPUTATIONAL FLUID DYNAMICS CODES; CRANKED-ARROW WING; DELAYED-DETACHED EDDY SIMULATION; DETACHED EDDY SIMULATIONS; PREDICTIVE CAPABILITIES; REYNOLDS - AVERAGED NAVIER-STOKES; STEADY AND UNSTEADY VISCOUS FLOWS;

SUPERSONIC AIRCRAFT;

EID: 63349111617     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.35163     Document Type: Article

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