DES grid resolution issues for vortical flows on a delta wing and an F-18C

41st Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2003, Pages

  Morton, Scott A ^a   Steenman, Matthew B ^a   Cummings, Russell M ^a   Forsythe, James R ^a  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT SIMULATORS; FLOW FIELDS; FLOW SEPARATION; MESH GENERATION; NASA; NUMERICAL ANALYSIS; SUPERSONIC AIRCRAFT; TURBULENT FLOW; VORTEX FLOW; WIND TUNNELS; WINGS;

ADAPTIVE MESH REFINEMENT; COMPLEX CONFIGURATION; DETACHED EDDY SIMULATIONS; LEADING EDGE EXTENSION; MASSIVELY SEPARATED FLOW; UNSTEADY PRESSURES; UNSTRUCTURED GRID; VORTICAL FLOWFIELDS;

DELTA WING AIRCRAFT;

EID: 85088719968     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-1103     Document Type: Conference Paper

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