Experimental investigation of circulation control on a shrouded fan

21st AIAA Applied Aerodynamics Conference

Volumn , Issue , 2003, Pages

  Kondor, Shayne A ^a   Lee, Warren ^a   Englar, Robert J ^a   Moore, Mark D ^b  

^a GEORGIA TECH RESEARCH INSTITUTE   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIR CUSHION VEHICLES; EFFICIENCY; FIGHTER AIRCRAFT; FLIGHT ENVELOPES; GROUND EFFECT; NASA; PNEUMATICS; ROCKET NOZZLES;

CIRCULATION CONTROL; CONVERGING NOZZLES; EXPERIMENTAL INVESTIGATIONS; IMPINGING PRESSURE; NASA LANGLEY RESEARCH CENTER; PERSONAL AIR VEHICLES; PROPULSIVE EFFICIENCIES; RESEARCH INSTITUTES;

NOZZLE DESIGN;

EID: 85067320688     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-3409     Document Type: Conference Paper

References (7)

1. McCormick, B., Aerodynamics of V/STOL Flight, Academic Press 1967.
2. Morel, J., Lissaman P., The Jet Flap Diffuser: A New Thrust Augmenting Device; AIAA Paper 69-777, July 1969.
3. Kondor S., Heiges, M., Active Flow Control for Control of Ducted Rotor Systems, AIAA Paper 2001-0117, Jan. 2001.
4. Englar, R. J., Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modification; Past, Present & Future, AIAA Paper 2000-2541.
5. TDI Model 457 Fan Manual, Tech Development Inc.
6. Lowe, H, et al, Static Performance of a 13.97cm (5.5 in) Diameter Model VTOL Lift Fan, NASA CR 2501, May 1972.
7. Englar, R. J., William R. M., Test Techniques for High Lift, Two-Dimensional Airfoils with Boundary Layer and Circulation Control for Application to Rotary Wing Aircraft, Canadian Aeronautics and Space Journal, Vol. 19, No. 3, March 1973.