Download reduction on a three dimensional V-22 model using active flow control

1st Flow Control Conference

Volumn , Issue , 2002, Pages

  Grife, R ^a   Darabi, A ^a   Wygnanski, I ^a,b,c  

^a University of Arizona   (United States)

^b TEL AVIV UNIVERSITY   (Israel)

^c UNIVERSITY OF ARIZONA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

CONVERTIBLE HELICOPTERS; FOUNTAINS; WINGS;

ACTIVE FLOW CONTROL; FLOW CHARAC-TERISTICS; FOUNTAIN FLOW; IMAGE PLANE; TEST AND EVALUATION; THREE-DIMENSIONAL MODEL; TILT ROTOR; TWO SOURCES;

FLOW CONTROL;

EID: 85087193312     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2002-3071     Document Type: Conference Paper

References (7)

1. Wood TL, Peryea MA "Reduction of Tilt Rotor Download" J AM HELICOPTER SOC 40 (3): 42-51 JUL 1995.
2. McVeigh M et al "Tiltrotor download reduction using Advanced Flow Control Techniques" AM HELICOPTOR SOC ARLINGTON 2001 00-16.
3. Kjellgren P, Anderberg N, and Wygnanski I "Download Allieviation by periodic excitation on a typical Tiltrotor configuration - Computation and Experiment" Denver 2000, AIAA 2000-2697.
4. Felker FF, Light JS "Rotor/Wing Aerodynamic Interactions in Hover" NASA Technical Memorandum 88255, May 1986.
5. Darabi, A., "On the mechanisms of forced flow reattachment", PhD thesis, Tel Aviv University 2001, Tel Aviv Israel.
6. Martin BP, Pugliese GJ, Leishman JG, "High resolution trailing vortex measurements in the wake of a hovering rotor", 56th Annual Forum of the American Helicopter Society, 2001.
7. Swanson AA, Light JS, "Shadowgraph flow visualization of isolated tiltrotor and rotor/wing wakes", 48th Annual Forum of the American Helicopter Society, 1992.