A new class of synthetic jet actuators - Part II: Application to flow separation control

Journal of Fluids Engineering, Transactions of the ASME

Volumn 127, Issue 2, 2005, Pages 377-387

  Gilarranz, J L ^a   Traub, L W ^a   Rediniotis, O K ^a  

^a Texas AandM University   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW CONTROL; FLOW VISUALIZATION; JETS; REYNOLDS NUMBER; WIND TUNNELS; WINGS;

FLOW SEPARATION CONTROL; FORCE BALANCE MEASUREMENTS; SURFACE PRESSURE MEASUREMENTS; SYNTHETIC JET ACTUATORS (SJA);

ACTUATORS;

EID: 20444446000     PISSN: 00982202     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.1882393     Document Type: Article

References (35)

1. Chang, P. K., 1976, Control of Flow Separation, Hemisphere Publishing, Washington, DC, pp. 1-84, 154-412.
2. Gad-el-Hak, M., and Bushnell, D., 1991, "Separation Control: Review," ASME J. Fluids Eng., 113, pp. 5-30.
3. Johnson, W. S., Tennant, J. S., and Stamps, R. E., 1975, "Leading-Edge Rotating Cylinder for Boundary Layer Control on Lifting Surfaces," AIAA Journal Hydronautics, 9, pp. 76-78.
4. Mokhtarian, F., and Modi, V. J., 1988, "Fluid Dynamics of Airfoils With Moving Surface Boundary-Layer Control," J. Aircr., 25, pp. 163-169.
5. Modi, V. J., Mokhtarian, F., Fernando, M., and Yokomizo, T., 1989, "Moving Surface Boundary Layer Control as Applied to 2-D Airfoils," AIAA Paper No. 89-0296.
6. Alvarez-Calderon, A., 1964, "Rotating Cylinder Flaps of V/STOL Aircraft," Aircraft Engineering, 36, pp. 304-309.
7. Gad-el-Hak, M., 2000, Flow Control: Passive, Active, and Reactive Flow Management, Cambridge University Press, New York, pp. 150-188.
8. Englar, R. J., 2000, "Circulation Control Pneumatic Aerodynamics: Blown Force and Moment Augmentation and Modification; Past, Present and Future," AIAA Paper No. 2000-2541.
9. McManus, K., Ducharme, A., Goldey, C., and Magil, J., 1996, "Pulsed Jet Actuators for Suppressing Flow Separation," AIAA Paper No. 96-0442.
10. McManus, K., and Magil, J., 1997, "Airfoil Performance Enhancement Using Pulsed Jet Separation Control," AIAA Paper No. 97-1971.
11. Huang, L. S., Maestrello, L., and Briant, T. D., 1987, "Separation Control Over an Airfoil at High Angles of Attack by Sound Emanating From the Surface," AIAA Paper No. 87-1261.
12. Hsiao, F. B., Liu, C. F., and Shyu, J. Y., 1990, "Control of Wall Separated Flow by Internal Acoustic Excitation," AIAA J., 28, pp. 1440-1446.
13. Koga, D. J., Reisenthel, P., and Nagib, H. M., 1984, "Control of Separated Flowfields Using Forced Unsteadiness," Fluids and Heat Transfer Report No. R-84-1, Illinois Institute of Technology, Chicago, IL.
14. Bar-Sever, A., 1989, "Separation Control on an Airfoil by Periodic Forcing," AIAA J., 27, pp. 820-821.
15. Lachman, G. V., 1961, Boundary Layer and Flow Control, Pergamon Press, Oxford, Great Britain, Vols. 1 and 2.
16. Gad-el-Hak, M., 1990, "Control of Low-Speed Airfoil Aerodynamics," AIAA J., 28, pp. 1537-1552.
17. Greenblatt, D., and Wygnanski, I., 1998, "Dynamic Stall Control by Oscillatory Forcing," AIAA Paper No. 98-0676.
18. Greenblatt, D., Darabi, A., Nishri, B., and Wygnanski, I., 1998, "Separation Control By Periodic Addition of Momentum With Particular Emphasis on Dynamic Stall," Proceedings Heli Japan 98, Paper T3-4, American Helicopter Society.
19. Seifert, A., and Pack, L., 1999b, "Oscillatory Excitation of Unsteady Compressible Flows Over Airfoils at Flight Reynolds Number," AIAA Paper No. 99-0925.
20. Pack, L., and Seifert, A., 2000, "Dynamics of Active Separation Control at High Reynolds Numbers," AIAA Paper No. 2000-0409.
21. Seifert, A., and Pack, L., 2000, "Separation Control at Flight Reynolds Numbers: Lessons Learned and Future Directions," AIAA Paper No. 2000-2542.
22. Donovan, J. F., Kral, L. D., and Cary, A. W., 1998, "Active Flow Control Applied to an Airfoil," AIAA Paper No. 98-0210.
23. Hassan, A., and Munts, E. A., 2000, "Transverse and Near-Tangential Synthetic Jets for Aerodynamic Flow Control," AIAA Paper No. 2000-4334.
24. He, Y., and Kral, L., 2000, "Post-Stall Control on an Airfoil Using Localized Jet Actuators," AIAA Paper No. 2000-0408.
25. He, Y., Cary, A. W., and Peters, D. A., 2001, "Parametric and Dynamic Modeling for Synthetic Jet Control of a Post-Stall Airfoil," AIAA Paper No. 2001-0733.
26. Amitay, M., Smith, B. L., and Glezer, A., 1998, "Aerodynamic Flow Control Using Synthetic Jet Technology," AIAA Paper No. 98-0208.
27. Honohan, A. M., Amitay, M., and Glezer, A., 2000, "Aerodynamic Control Using Synthetic Jets," AIAA Paper No. 2000-2401.
28. Parekh, D. E., and Glezer, A., 2000, "AVIA: Adaptive Virtual Aerosurface," AIAA Paper No. 2000-2474.
29. Smith, B. L., and Glezer, A., 1997, "Vectoring and Small-Scale Motions Effected in Free Shear Flows Using Synthetic Jet Actuators," AIAA Paper No. 97-0213.
30. Smith, B. L., Trautman, M. A., and Glezer, A., 1999, "Controlled Interactions of Adjacent Synthetic Jets," AIAA Paper No. 99-0669.
31. Pack, L., and Seifert, A., 1999, "Periodic Excitation for Jet Vectoring and Enhanced Spreading," AIAA Paper No. 99-0672.
32. Rae, W., and Pope, A., 1984, Low Speed Wind Tunnel Testing, Wiley, New York, pp. 199-208, 362-424.
33. Gilarranz, J. L., 2001, "Development of High-Power, Compact Synthetic Jet Actuators for Flow Separation Control," Ph.D. dissertation, Texas A&M University, Texas.
34. Traub, L. W., 1992, "A Subsonic Wind-Tunnel Investigation of the Effect of Sharp Edged Sheared Tips on a Moderate Aspect Ratio Flat Plate Wing," M.S. thesis. University of the Witwatersrand, Johannesburg, South Africa.
35. Summers, J. L., and Page, W. A., 1950, "Lift and Moment Characteristics at Subsonic Mach Numbers of Four 10-Percent-Thick Airfoil Sections of Varying Trailing-Edge Thickness," NACA R. M. A50J09, NACA, Washington D.C.