Some aspects of aerodynamic flow control using synthetic-jet actuation

Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences

Volumn 369, Issue 1940, 2011, Pages 1476-1494

  Glezer, Ari ^a  

^a GEORGIA INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

Flow control; Synthetic jets; Trapped vorticity

Indexed keywords

FLOW CONTROL; JETS; LOCOMOTIVES; RAILROAD CARS; VORTICITY;

ACTIVE FLOW CONTROL; ACTUATION TIME; AERODYNAMIC FLOW CONTROL; AERODYNAMIC FORCES; AERODYNAMIC SHAPE; AEROFOILS; BASEFLOWS; BLUFF BODY; CROSS FLOWS; FLOW BOUNDARIES; FLOW SYSTEMS; GLOBAL INSTABILITY; INHERENT INSTABILITY; JET ACTUATORS; LIFTING SURFACES; MASS INJECTION; ORDERS OF MAGNITUDE; QUASI-STEADY; SEPARATED FLOWS; SPATIAL SCALE; SYNTHETIC JETS; TIME-SCALES; TRAPPED VORTICITY; VORTICAL STRUCTURES; ZERO-NET-MASS-FLUX;

AERODYNAMICS;

EID: 79954468589     PISSN: 1364503X     EISSN: None     Source Type: Journal    
DOI: 10.1098/rsta.2010.0374     Document Type: Review

References (71)

1. Smith, B. L. & Glezer, A. 1998 The formation and evolution of synthetic jets. Phys. Fluids 10, 2281-2297. (doi:10.1063/1.869828) (Pubitemid 128591615)
2. Yao, C. S., Chen, F. J. & Neuhart, D. 2006 Synthetic jet flowfield database for computational fluid dynamics validation. AIAA J. 44, 3153-3157. (doi:10.2514/1.13819) (Pubitemid 46065094)
3. Cater, J. E. & Soria, J. 2002 The evolution of round zero-net-mass-flux jets. J. Fluid Mech. 472, 167-200. (doi:10.1017/ S0022112002002264) (Pubitemid 36022115)
4. Shuster, J. M. & Smith, D. R. 2007 Experimental study of the formation and scaling of a round synthetic jet. Phys. Fluids 19, 045109. (doi:10.1063/1.2711481) (Pubitemid 46705906)
5. Rizzetta, D. P., Visbal, M. R. & Stanek, M. J. 1999 Numerical investigation of synthetic-jet flow fields. AIAA J. 37, 919-927. (doi:10.2514/2.811)
6. Lee, C. Y. & Goldstein, D. B. 2002 Two-dimensional synthetic jet simulation. AIAA J. 40, 510-516. (doi:10.2514/2.1675) (Pubitemid 34554611)
7. Kotapati, R. Mittal, R. & Cattafesta, L. 2007 Numerical simulation of a transitional synthetic jet in quiescent external flow. J. Fluid Mech. 581, 287-321. (doi:10.1017/S0022112007005642) (Pubitemid 47304515)
8. Yamaleev, N. K. & Carpenter, M. H. 2006 Quasi-one-dimensional model for realistic threedimensional synthetic jet actuators. AIAA J. 44, 208-216. (doi:10.2514/1.14495)
9. Gallas, Q., Holman, R., Nishida, T., Carroll, B., Sheplak, M. & Cattafesta, L. 2003 Lumpedelement modeling of piezoelectric-driven synthetic jet actuators. AIAA J. 41, 240-247. (doi:10.2514/2.1936)
10. Watson, M. A., Jaworski, J. & Wood, N. J. 2003 A study of synthetic jets from rectangular and dual-circular orifices. Aero J. 107, 427-434.
11. Smith, B. L. & Glezer, A. 2005 Vectoring of adjacent synthetic jets. AIAA J. 43, 2117-2124. (doi:10.2514/1.12910) (Pubitemid 41498948)
12. Tang, H. & Zhong, S. 2007 A static compressible flow model of synthetic jet actuators. Aero J. 111, 421-431. (Pubitemid 47388711)
13. Crittenden, T. M. & Glezer, A. 2006 A high-speed, compressible synthetic jet. Phys. Fluids 18, 017107. (doi:10.1063/1.2166451)
14. Zhong, S., Millet, F. & Wood, N. J. 2005 The behaviour of circular synthetic jets in a laminar boundary layer. Aero J. 109, 461-470. (Pubitemid 41680304)
15. Liddle, S. C. & Wood, N. J. 2005 Investigation into clustering of synthetic jet actuators for flow separation control applications. Aero J. 109, 35-44. (Pubitemid 40359771)
16. Jabbal, M. & Zhong, S. 2008 The near wall effect of synthetic jets in a boundary layer. Int. J. Heat Fluid Flow 29, 119-130. (doi:10.1016/j. ijheatfluidflow.2007.07.011)
17. Jabbal, M. & Zhong, S. 2010 Particle image velocimetry measurements of the interaction of synthetic jets with a zero-pressure gradient laminar boundary layer. Phys. Fluids 22, 063603. (doi:10.1063/1.3432133)
18. Milanovic, I. M. & Zaman, K. B. M. Q. 2005 Synthetic jets in crossflow. AIAA J. 43, 929-940. (doi:10.2514/1.4714) (Pubitemid 40701481)
19. Smith, D. R. 2002 Interaction of a synthetic jet with a cross flow boundary layer. AIAA J. 40, 2277-2288. (doi:10.2514/2.1564) (Pubitemid 35361049)
20. Dandois, J. & Garnier, E. 2006 Unsteady simulation of a synthetic jet in a crossflow. AIAA J. 44, 225-238. (doi:10.2514/1.13462)
21. Rumsey, C. L., Gatski, T. B., Sellers III, W. L., Vatsa, V. N. & Viken, S. A. 2006 Summary of the 2004 computational fluid dynamics validation workshop on synthetic jets. AIAA J. 44, 194-207. (doi:10.2514/1.12957)
22. Rathnasingham, R. & Breuer, K. S. 2003 Active control of turbulent boundary layers. J. Fluid Mech. 495, 209-233. (doi:10.1017/S0022112003006177) (Pubitemid 38025063)
23. Wu, J.-Z., Lu, X.-Y., Denny, A. G., Fan, M. & Wu, J.-M. 1998 Post stall flow control on an airfoil by local unsteady forcing. J. Fluid Mech. 371, 21-58. (doi:10.1017/S0022112098002055) (Pubitemid 128483439)
24. Ahuja, K. K. & Burrin, R. H. 1984 Control of flow separation by sound. In 9th Aeroacoustics Conf., Williamsburg, VA, 15-17 October 1984. American Institute of Aeronautics and Astronautics (AIAA) paper 1984-2298.
25. Hsiao, F.-B., Liu, C.-F. & Shyu, J.-Y. 1990 Control of wall-separated flow by internal acoustic excitation. AIAA J. 28, 1440-1446. (doi:10.2514/3.25236)
26. Seifert, A., Bachar, T., Koss, D., Shepshelovich, M. & Wygnanski, I. 1993 Oscillatory blowing: a tool to delay boundary layer separation. AIAA J. 31, 2052-2060. (doi:10.2514/3.49121)
27. Amitay, M. & Glezer, A. 2002 Role of actuation frequency in controlled flow reattachment over a stalled airfoil. AIAA J. 40, 209-216. (doi:10.2514/2.1662) (Pubitemid 34172832)
28. Amitay, M. & Glezer, A. 2002 Controlled transients of flow reattachment over stalled airfoils. Int. J. Heat Fluid Flow 23, 690-699. (doi:10.1016/S0142-727X(02)00165-0) (Pubitemid 34878040)
29. Glezer, A., Amitay, A. & Honohan, A. 2005 Aspects of low- and high-frequency actuation for aerodynamic flow control. AIAA J. 43, 1501-1511. (doi:10.2514/1.7411) (Pubitemid 41013797)
30. Greenblatt, D. 2006 Managing flap vortices via separation control. AIAA J. 44, 2755-2764. (doi:10.2514/1.19664) (Pubitemid 44788072)
31. Greenblatt, D. & Wygnanski, I. J. 2001 Use of periodic excitation to enhance airfoil performance at low reynolds numbers. J. Aircraft 38, 190-192. (doi:10.2514/2.2752) (Pubitemid 32253148)
32. Margalit, S., Greenblatt, D., Seifert, A. & Wygnanski, I. 2005 Delta wing stall and roll control using segmented piezoelectric fluidic actuators. J. Aircraft 42, 698-709. (doi:10.2514/1.6904) (Pubitemid 41013371)
33. Raju, R., Mittal, R. & Cattafesta, L. 2008 Dynamics of airfoil separation control using zero-net mass-flux forcing. AIAA J. 46, 3103-3115. (doi:10.2514/1.37147)
34. You, D., Ham, F. & Moin, P. 2008 Discrete conservation principles in large-eddy simulation with application to separation control over an airfoil. Phys. Fluids 20, 101515. (doi:10.1063/1.3006077)
35. Gilarranz, J. L., Traub, L. W. & Rediniotis, O. K. 2005 A new class of synthetic jet actuators: application to flow separation control. J. Fluids Eng. 127, 377-387. (doi:10.1115/1.1882393) (Pubitemid 40819401)
36. Smith, D.M., Dickey, E. & VonKlein, T. 2006 The ADVINT program. In 3rd AIAA Flow Control Conf., San Francisco, CA, 5-8 June 2006. AIAA paper 2006-2854.
37. Shmilovich, A. & Yadlin, Y. 2006 Flow control for the systematic buildup of high lift systems. In 3rd AIAA Flow Control Conf., San Francisco, CA, 5-8 June 2006. AIAA paper 2006-2855.
38. Ho, C.-M. & Huang, L.-S. 1982 Subharmonics and vortex merging in mixing layers. J. Fluid Mech. 119, 443-473. (doi:10.1017/S0022112082001438)
39. Unal, M. & Rockwell, D. 1988 On vortex formation from a cylinder. I. The initial instability. J. Fluid Mech. 190, 491-512. (doi:10.1017/ S0022112088001429)
40. Wu, J.-Z., Lu, X.-Y., Denny, A. G., Fan, M. & Wu, J.-M. 1998 Post-stall control on an airfoil by local unsteady forcing. J. Fluid Mech. 371, 21-58. (doi:10.1017/S0022112098002055) (Pubitemid 128483439)
41. Chang, P. K. 1976 Control of flow separation. New York, NY: McGraw-Hill.
42. Perkins, D. C. & Hazen, D. C. 1953 Some recent advances in boundary layer and circulation control. In 4th Anglo-American Aero. Conf. (eds J. Bradbrooke & E. C. Pike), pp. 189-224. New York, NY: AIAA.
43. Ringleb, F. O. 1961 Separation control by trapped vortices. In Boundary layer flow control (ed. G. V. Lachmann), pp. 265-294. New York, NY: Pergamon Press.
44. Hurley, D. G. 1961 The use of boundary layer control to establish free stream-line flows. In Boundary layer flow control (ed. G. V. Lachmann), pp. 295-341. New York, NY: Pergamon Press.
45. Roshko, A. & Fizdon, W. 1969 On the persistence of transition in the near wake. In Problems of Hydrodynamics and Continuum Mechanics, pp. 606-616. Philadelphia, PA: SIAM, Philadelphia.
46. Roshko, A. 1993 Perspectives on bluff body aerodynamics. J. Wind Eng. Indust. Aero. 49, 79-100. (doi:10.1016/0167-6105(93)90007-B)
47. Schewe, G. 1986 Sensitivity of transition phenomena to small perturbations in flow round a circular cylinder. J. Fluid Mech. 172, 33-46. (doi:10.1017/S0022112086001635) (Pubitemid 17512288)
48. Roshko, A. 1961 Experiments on the flow past a circular cylinder at very high reynolds number. J. Fluid Mech. 10, 345-356. (doi:10.1017/ S0022112061000950)
49. Schlichting, H. 1968 Boundary layer theory, 6th edn. New York, NY: McGraw-Hill.
50. Fage, A. & Warsap, J. H. 1929 The effects of turbulence and surface roughness on the drag of a circular cylinder. Aeronautical Research Committee Reports and Memoranda no. 1283.
51. James, D. F. & Truong, Q.-S. 1972 Wind load on cylinder with spanwise protrusion. J. Eng. Mech. Div. 98, 1573-1589.
52. Glezer, A. & Amitay, M. 2002 Synthetic jets. Annu. Rev. Fluid Mech. 34, 503-529. (doi:10.1146/ annurev.fluid.34.090501.094913) (Pubitemid 35372032)
53. Honohan, A. M. 2003 The interaction of synthetic jets with cross flow and the modification of aerodynamic surfaces. PhD thesis, Georgia Institute of Technology, Atlanta, USA.
54. Honohan, A. M., Amitay, M. & Glezer, A. 2000 Aerodynamic control using synthetic jets. In 31st AIAA Fluid Dynamics Conf. and Exhibit, Denver, CO, 19-22 June 2000. AIAA paper 2000-2401.
55. Mittal, R. & Rampunggoon, P. 2002 On the virtual aeroshaping effect of synthetic jets. Phys. Fluids 14, 1533-1536. (doi:10.1063/1.1453470) (Pubitemid 34439834)
56. Amitay, M., Horvath, M., Michaux, M. & Glezer, A. 2001 Virtual aerodynamic shape modification at low angles of attack using synthetic jet actuators. In 31st AIAA Fluid Dynamics Conf. and Exhibit, Anaheim, CA, 11-14 June 2001. AIAA paper 2001-2975.
57. Amitay, M., Smith, D. R., Kibens, V., Parekh, D. E. & Glezer, A. 2001 Aerodynamic flow control over an unconventional airfoil using synthetic jet actuators. AIAA J. 39, 361-370. (doi:10.2514/2.1323) (Pubitemid 32255392)
58. Timor, I., Ben-Hamou, E., Guy, Y. & Seifert, A. 2004 Maneuvering aspects and 3D effects of active airfoil flow control. In 2nd AIAA Flow Control Conf., Portland, OR, 28-31 June 2004. AIAA paper 2004-2614.
59. Watson, M., Jaworski, A. J. & Wood, N. J. 2007 Application of synthetic jet actuators for the modification of the characteristics of separated shear layers on slender wings. Aero J. 111, 519-530.
60. Rehman, A. & Kontis, K. 2006 Synthetic jet control effectiveness on stationary and pitching airfoils. J. Aircraft 43, 1782-1789. (doi:10.2514/1.20333) (Pubitemid 46065242)
61. Chatlynne, E., Rumigny, N., Amitay, M. & Glezer, A. 2001 Virtual aero-shaping of a clarky airfoil using synthetic jet actuators. In 39th Aerospace Sciences Meeting and Exhibit, Reno, NV, 8-11 January 2001. AIAA paper 2001-0732.
62. DeSalvo, D. M. & Glezer, A. 2004 Aerodynamic performance modification at low angles of attack by trailing edge vortices. In 2nd AIAA Flow Control Conf., Portland, OR, 28-31 June 2004. AIAA paper 2004-2118.
63. DeSalvo, D. M. & Glezer, A. 2005 Airfoil aerodynamic performance modification using hybrid surface actuators. In 43rd AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 10-13 January 2005. AIAA paper 2005-0872.
64. DeSalvo, D. M. & Glezer, A. 2007 Control of airfoil aerodynamic performance using distributed trapped vorticity. In 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 8-11 January 2007. AIAA paper 2007-0708.
65. Muse, J., Kutay, A., Brzozowski, D., Culp, J., Calise, A. & Glezer, A. 2008 Dynamic flight maneuvering using trapped vorticity flow control. In 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 7-10 January 2008. AIAA paper 2008-522.
66. Szepessy, S. & Bearman, P. W. 1992 Aspect ratio and end plate effects on vortex shedding from a circular cylinder. J. Fluid Mech. 234, 191-217. (doi:10.1017/S0022112092000752)
67. Tensi, J., Boué, I., Paillé, F. & Dury, G. 2002 Modification of the wake behind a circular cylinder by using synthetic jets. J. Visualization 5, 37-44. (doi:10.1007/BF03182601)
68. Ekmekci, A. & Rockwell, D. 2010 Effects of a geometrical surface disturbance on flow past a circular cylinder: a large scale spanwise wire. J. Fluid Mech. 665, 120-157. (10.1017/S0022112010003848)
69. DeSalvo, D. M. & Glezer, A. 2006 Aerodynamic control at low angles of attack using trapped vorticity concentrations. In 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, 9-12 January 2006. AIAA paper 2006-0100.
70. Brzozowski, D. P., Culp, J. R., Kutay, A. T., Muse, J. A. & Glezer, A. 2008 Closed-loop aerodynamic flow control of a free airfoil. In 4th Flow Control Conf., Seattle, WA, 23-26 June 2008. AIAA paper 2008-4323.
71. Brzozowski, D. P. & Glezer, A. 2008 Aerodynamic closed-loop flow control of a free-moving airfoil using trapped vorticity. In Int. Conf. on Jets, Wakes and Separated Flows, Berlin, Germany, 16-19 September 2008.