Detached-eddy simulation of the vortical flowfield about the VFE-2 deltaWing

46th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2008, Pages

  Cummings, Russell M ^a   Schütte, Andreas ^b  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

DELTA WINGS; DETACHED EDDY SIMULATIONS; EXPERIMENTAL DATA; FLOW TOPOLOGY; HYBRID APPROACH; HYBRID MESHES; LEADING EDGE; NUMERICAL RESEARCH; NUMERICAL RESULTS; NUMERICAL SIMULATION; PRESSURE SENSITIVE PAINTS; PRIMARY VORTEX; RANS EQUATION; REYNOLDS NUMBER EFFECT; SURFACE PRESSURES; WORKING GROUPS;

AEROSPACE ENGINEERING; COBALT; COMPUTER SIMULATION; DELTA WING AIRCRAFT; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER;

MATHEMATICAL MODELS;

EID: 78149460551     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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