Analysis of PSP results obtained for the VFE-2 65° delta wing configuration at sub- And transonic speeds

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 2, Issue , 2006, Pages 777-797

  Konrath, Robert ^a   Klein, Christian ^a   Engler, Rolf H ^a   Otter, Dirk ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

DATA ACQUISITION; DELTA WING AIRCRAFT; MACH NUMBER; NASA; PRESSURE SENSORS; SUBSONIC AERODYNAMICS; TRANSONIC AERODYNAMICS; VORTEX FLOW; WIND TUNNELS;

FLOW TOPOLOGY; INNER PRIMARY VORTEX.; NEW WIND-TUNNEL TESTS; OUTER PRIMARY VORTEX; PRESSURE SENSITIVE PAINT; VORTEX BREAKDOWN;

AEROSPACE ENGINEERING;

EID: 34250759802     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-60     Document Type: Conference Paper

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