Control of poststall airfoil aerodynamics based on surface perturbation

AIAA Journal

Volumn 46, Issue 10, 2008, Pages 2510-2519

  Zhang, M M ^a,b,c   Zhou, Y ^a,b   Cheng, L ^a,b  

^a HONG KONG POLYTECHNIC UNIVERSITY   (Hong Kong)

^b Department of Mechanical Engineering ^*

^c Johns Hopkins University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC EFFICIENCIES; AIRFOIL AERODYNAMICS; AIRFOIL STALLS; CONTROL SIGNALS; DRAG RATIOS; EXPERIMENTAL INVESTIGATIONS; FIGURE OF MERITS; HOT WIRES; LASER DOPPLER ANEMOMETERS; LIFT AND DRAGS; LIFT COEFFICIENTS; LOAD CELLS; LOCAL SURFACES; LOOP CONTROL SYSTEMS; NACA0012 AIRFOILS; PARTICLE IMAGE VELOCIMETRY; PIEZOCERAMIC ACTUATORS; POSTSTALL AIRFOILS; SINE WAVES; SURFACE PERTURBATIONS; WAVE EXCITATIONS;

AERODYNAMICS; AIR; CONTROL SYSTEMS; DRAG; DYNAMICS; FLOW VISUALIZATION; GAS DYNAMICS; PERTURBATION TECHNIQUES;

AIRFOILS;

EID: 54549107838     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/1.35792     Document Type: Article

References (35)

1. Anderson, J. D., Jr., Intraduction to Flight, McGraw-Hill, New York, 2005.
2. Schlichting, H., Boundary Laver Theory, McGraw-Hill, New York, 1979.
3. Gad-el-Hak, M., and Bushnell, D. M., "Separation Control: Review," Journal of Fluids Engineering, Vol 113, No. 1, 1991, pp. 5-30.
4. Greenblatt, D., and Wygnanski, I. J., "Control of Flow Separation by Periodic Excitation," Progress in Aerospace Sciences, Vol. 36, No. 7, 2000. pp. 487-545. doi:10.1016/S0376-0421(00)00008-7
5. Corke, T., Design of Aircraft, Prentice-Hall, New York, 2002.
6. Modi, V. J., Hill, S. S., and Yokomizo, T., "Drag Reduction of Trucks Through Boundary-Layer Control," Journal of Wind Engineering and Industrial Aerodynamics, Vol. 54, No. 3, 1995, pp. 583-594. doi:10.1016/0167-6105(94)00074-N
7. Seifert, A., Darabi, A., and Wygnanski, I., "Delay of Airfoil Stall by Periodic Excitation," Journal of Aircraft, Vol. 33, No. 4, 1996, pp. 691-698.
8. 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.
9. Sinha, S. K., "Flow Separation Control with Microflexural Wall Vibrations," Journal of Aircraft, Vol. 38, No. 3, 2001, pp. 496-503.
10. Zaman, K. B. M. Q., Bar-Sever, A., and Mangalam, S. M., "Effect of Acoustic Excitation on the Flow over a Low-Re Airfoil," Journal of Fluid Mechanics, Vol. 182, No. 1, 1987, pp. 127-148. doi:10.1017/ S0022112087002271
11. Hsiao, F. B., Liu, C. F., and Shyu, J. Y., "Control of Wall-Separated Flow by Internal Acoustic Excitation," AIAA Journal, Vol. 28, No. 8, 1990, pp. 1440-1446.
12. Seifert, A., Eliahu, S., Greenblatt, D., and Wygnanski, I., "Use of Piezoelectric Actuators for Airfoil Separation Control," AIAA Journal, Vol. 36, No. 8, 1998, pp. 1535-1537.
13. Melton, L. P., Schaeffler, N. W., Yao, C. S., and Seifert, A., "Active Control of Flow Separation from Supercritical Airfoil Leading-Edge Flap Shoulder," Journal of Aircraft, Vol. 42, No. 5, 2005, pp. 1142-1149. doi:10.2514/1.10294
14. Cheng, L., Zhou, Y., and Zhang, M. M., "Perturbed Interaction Between Vortex Shedding and Induced Vibration," Journal of Fluids and Structures, Vol. 17, No. 7, 2003, pp. 887-901. doi:10.1016/S0889-9746(03) 00042-2
15. Zhang, M. M., Cheng, L., and Zhou, Y., "Closed-Loop-Controlled Vortex Shedding from a Flexibly Supported Square Cylinder Under Different Schemes," Physics of Fluids, Vol. 16, April 2004, pp. 1439-1448. doi:10.1063/1.1687413
16. Zhang, M. M., Cheng, L., and Zhou, Y., "Closed-loop controlled vortex-airfoil interactions," Physics of Fluids, Vol. 18, April 2006, p. 046102. doi:10.1063/1.2189287
17. Huang, J. F., Zhou, Y., and Zhou, T. M., "Three-Dimensional Wake Structure Measurement Using a Modified PIV Technique," Experiments in Fluids, Vol 40, No. 6, 2006, pp. 884-896. doi:10.100/s00948-006-0126-9
18. Hoarau, Y., Braza, M., Ventikos, Y., Faghani, D., and Tzabiras, G., "Organized Modes and the Three-Dimensional Transition to Turbulence in the Incompressible Flow Around a NACA0012 Wing," Journal of Fluid Mechanics, Vol. 496. Dec. 2003, pp. 63-72. doi:10.1017/S0022112003006530
19. Copeland, B. M., Buckley, J. D., Bryant, R. G., Fox, R. L., and Hellbaum, R. F., "THUNDER: An Ultra-High Displacement Piezoelectric Actuator," NASA Langley Research Center, VA 23681-0001, 1999.
20. Wise, S. A., "Displacement Properties of RAINBOW and THUNDER Piezoelectric Actuators," Sensors and Actuators A (Physical), Vol. 69, No 1, 1998, pp. 33-38. doi:10.1016/S0924-4247(97)01745-7
21. Zhang, M. M., Zhou, Y., and Cheng, L., "Spring-Supported Cylinder Wake Control," AIAA Journal, Vol. 41, No. 8, 2003, pp. 1500-1506.
22. Maskell, E. C., "Theory of the Blockage Effects on Bluff Bodies and Stalled Wings in a Closed Wind Tunnel," Aeronautical Research Council Repts. and Memo., No. 3400, Nov. 1963.
23. Michos, A., Bergeles, G., and Athanassiadis, N., "Aerodynamic Characteristics of NACA0012 Airfoil in Relation to Wind Generators," Wind Engineering, Vol. 7, No. 4, 1983, pp. 247-262.
24. Wu, J. Z., Lu, X. Y., Denny, A. G., Fan, M., and Wu, J. M., "Post-Stall Flow Control on an Airfoil by Local Unsteady Forcing," Journal of Fluid Mechanics, Vol. 371, April 1998, pp. 21-58. doi:10.1017/S0022112098002055
25. Margalit, S., Greenblatt, D., Seifert, A., and Wygnanski, I., "Delta Wing Stall and Roll Control Using Segmented Piezoelectric Fluidic Actuators," Journal of Aircraft, Vol. 42, No. 3, 2005, pp. 698-709. doi:10.2514/1.6904
26. Amitay, M., Smith, D. R., Kibens, V., Parekh, D. E., and Glezer, A., "Aerodynamic Flow Control over an Unconventional Airfoil Using Synthetic Jet Actuators," AIAA Joumal, Vol. 39, No. 3, 2001, pp. 361-370.
27. Bons, J. P., Sondergaard, R., and Rivir, R. B., "Fluid Dynamics of LPT Blade Separation Control Using Pulsed Jets," Journal of Turbomachinery, Vol. 124, No. 1, 2002, pp. 77-85. doi:10.1115/1.1425392
28. Dandois, J., Gamier, E., and Sagaut, P., "Numerical Simulation of Active Separation Control by a Synthetic Jet," Journal of Fluid Mechanics, Vol. 574, Feb. 2007, pp. 25-58. doi:10.1017/S0022112006003995
29. Amitay, M., and Giezer, A., "Role of Actuation Frequency in Controlled Flow Reattachment over Stalled Airfoil," AIAA Journal, Vol. 40, No. 2, 2002, pp. 203-216.
30. Glezer, A., Amitay, M., and Honohan, A. M., "Aspects of Low- and High-Frequency Aerodynamics Flow Control," AIAA Journal, Vol. 43, No. 7, 2005, pp. 1501-1511. doi:10.2514/1.7411
31. Bar-Sever, A., "Separation Control on an Airfoil by Periodic Forcing," AIAA Journal, Vol. 27, No. 6, 1989, pp. 820-821.
32. Cantwell, B. J., and Coles, D., "Experimental Study of Entrapment and Transport in the Turbulent Near Wake of a Circular Cylinder," Journal of Fluid Mechanics, Vol. 136, April 1983, pp. 321-374. doi:10.1017/S0022112083002189
33. Unal, M. F., and Rockwell, D., "On the Vortex Formation from a Cylinder, Part 1: The Initial Instability," Journal of Fluid Mechanics, Vol 190, April 1988. pp. 491-512. doi:10.1017/S0022112088001429
34. Zhang, M. M., Zhou, Y., and Cheng, L., "Closed-Loop-Manipulated Wake of a Stationary Square Cylinder," Experiments in Fluids, Vol. 39, No 1, 2005. pp. 75-85. doi:10.1007/s00348-005-0979-3
35. Katz, J., "Discrete Vortex Method for the Non-Steady Separated Flow over an Airfoil," Journal of Fluid Mechanics, Vol. 102, April 1981, pp. 315-328. doi:10.1017/S0022112081002668