The effects of leading edge suction on delta wing vortex breakdown

37th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1999, Pages

  Maines, Brant ^a   Moeller, Brian ^b   Rediniotis, Othon K ^b  

^a LOCKHEED MARTIN   (United States)

^b Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ANGLE OF ATTACK; ANGLE OF ATTACK INDICATORS; FLOW RATE; MILITARY VEHICLES; REYNOLDS NUMBER; RIVERS; VELOCITY MEASUREMENT; VORTEX FLOW; WINGS;

FREE-STREAM VELOCITY; HIGH-SPEED PARTICLES; LINEAR RELATIONSHIPS; SUCTION DISTRIBUTIONS; UNINHABITED COMBAT AIR VEHICLE; VISUAL MEASUREMENTS; VOLUMETRIC FLOW RATE; VORTEX BREAKDOWN CHARACTERISTICS;

DELTA WING AIRCRAFT;

EID: 84983097676     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1999-128     Document Type: Conference Paper

References (12)

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