Compressibility and excitation location effects on high Reynolds numbers active separation control

Journal of Aircraft

Volumn 40, Issue 1, 2003, Pages 110-119

  Seifert, Avi ^a   Pack, LaTunia G ^b  

^a TEL AVIV UNIVERSITY   (Israel)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; CRYOGENICS; DATA REDUCTION; KINEMATICS; REYNOLDS NUMBER; TURBULENCE;

BOUNDARY LAYER CONTROL (BLC); PERIODIC EXCITATIONS;

BOUNDARY LAYER FLOW;

EID: 0037224258     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/2.3065     Document Type: Article

References (11)

1. Betz, A., "History of Boundary Layer Control in Germany," Boundary Layer and Flow Control, Vol. 1, edited by G. V. Lachman, Pergamon Press, New York, 1961, p. 2.
2. Nishri, B., and Wygnanski, I., "Effect of Periodic Excitation on Turbulent Flow Separation from a Flap," AIAA Journal, Vol. 36, No. 4, 1998, pp. 547-556.
3. Seifert, A., Bachar, T., Koss, D., Shepshelovich, M., and Wygnanski, I., "Oscillatory Blowing, a Tool to Delay Boundary-Layer Separation," AIAA Journal, Vol. 31, No. 11, 1993, pp. 2052-2060.
4. Seifert, A., Darabi, A., and Wygnanski, I., "Delay of Airfoil Stall by Periodic Excitation," Journal of Aircraft, Vol. 33, No. 4, 1996, pp. 691-699.
5. Seifert, A., and Pack, L. G., "Oscillatory Control of Separation at High Reynolds Numbers," AIAA Journal, Vol. 37, No. 9, 1999, pp. 1062-1071.
6. Seifert, A., and Pack, L. G., "Oscillatory Control of Shock-Induced Separation," Journal of Aircraft, Vol. 38, No. 3, 2001, pp. 464-472.
7. Delery, J. M., "Shock Wave/Turbulent Boundary Layer Interaction and its Control," Progress in Aerospace Sciences, Vol. 22, 1985, pp. 209-280.
8. Seifert, A., and Pack, L. G., "Active Flow Separation Control on a Wall-Mounted Hump at High Reynolds Numbers," AIAA Journal, Vol. 40, No. 7, 2002, pp. 1363-2372.
9. Murthy, A. V., Johnson, C. B., Ray, E. J., Lawing, P. L., and Thibodeaux, J. L., "Studies of Sidewall Boundary Layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel With and Without Suction," NASA TP-2096, 1983.
10. Ladson, C. A., and Ray, E. J., "Evolution, Calibration, and Operational Characteristics of the Two-Dimensional Test Section of the Langley 0.3-Meter Transonic Cryogenic Tunnel," NASA TP-2749, 1987.
11. Rallo, R. A., Dress, D. A., and Siegle, H. J. A., "Operating Envelope Charts for the Langley 0.3-Meter Transonic Cryogenic Wind Tunnel," NASA TM-89008, 1986.