Pressure measurements and flow field visualization ob a delta wing with periodic blowing and suction

24th Atmospheric Flight Mechanics Conference

Volumn , Issue , 1999, Pages

  Guy, Yair ^a   Morrow, Julie A ^a   McLaughlin, Thomas E ^a   Wygnanski, Irael ^a,b  

^a UNITED STATES AIR FORCE ACADEMY   (United States)

^b TEL AVIV UNIVERSITY   (Israel)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANGLE OF ATTACK; FLOW CONTROL; HYDRAULIC STRUCTURES; LOCATION; PRESSURE DISTRIBUTION; REYNOLDS NUMBER; TUNNELS; VORTEX FLOW; WATER SUPPLY TUNNELS; WIND TUNNELS;

EXCITATION FREQUENCY; FLOWFIELD VISUALIZATION; FREE-STREAM VELOCITY; HIGH ANGLES OF ATTACK; LOW-SPEED WIND TUNNEL; MOMENTUM COEFFICIENT; NON-DIMENSIONAL FREQUENCY; VORTEX BREAKDOWN LOCATION;

DELTA WING AIRCRAFT;

EID: 84960539771     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Guy, Y., Morrow, J. A., MclaugHin, T. E-, "Control of Vortex Breakdown on a Delta Wiag by Periodic.Blowing and Suction", AIAA Paper 99­-0132, 1999.
2. Greenblat, D. and Wygnanski, L, "Dynamic Stall Control by Oscillatory: Forcing”, AIAA Paper 98­-0676, 1998.
3. Nishri, B., "On the Dominant Mechanisms Governing Active Control of Separation", PhD. Thesis, Tel-Aviv University, Israel
4. Nishri, B. and Wygnanski, I, "On the Flow Separation and its Control”, Computational Methods in Applied Science, 1996.
5. Seifert A., Darabi, A. and Wygnans M L, "Delay of Airfoil Stall by Periodic Excitation”, AIAA Journal of Aircraft, Vol. 33, No. 4, 1996.
6. Nave, T. "The Effect of Sweep on Separation Control over an Airfoil", M.Sc. Thesis, Tel-Aviv University, Israel, 1997.
7. Seifert, A., Darabi A. and Wygnanski, L, "The Effects of Forced Oscillations on the Performance of. Airfoils”, AIAA Paper 93-3264, 1993.
8. Wygnanski, L and Seifert, A., "The Control of Separation by Periodic Oscillations”, AIAA Paper 94-2608, 1994.