journal article·2012-08

Review of actuators for high speed active flow control

Lin Wang, ZhenBing Luo, ZhiXun Xia, Bing Liu, Xiong Deng

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Abstract

Actuators are one of the key points for the development of active flow control technology. Efficient methods of high speed flow control can provide enhanced propulsive efficiency and at the same time enable safe and maneuverable high speed flight. The development of high speed flight technology promotes the emergence of novel and robust actuators. This review introduces the state of the art in the development of actuators that can be used in high speed active flow control. The classification and different operation criteria of the actuators are discussed. The specifications, mechanisms and applications of various popular actuator types including fluidic, mechanical, and plasma actuators are described. Based on the realistic need of high speed flow control and the existing results of actuators, a new actuator design method is proposed. At last, the merits and drawbacks of the actuators are summarized and some suggestions on the development of active flow control technology are put forward.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Plasma and Flow Control in Aerodynamics · Aerodynamics and Fluid Dynamics Research · Fluid Dynamics and Turbulent Flows

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (100+)

Show source-provided references
1. Kumar, Hefner J N. Future challenges and opportunities in aerodynamics. ICAS 2000 Congress, 200010.1017/S0001924000064009 ↗
2. Zhuang F G, Huang Z C. The innovation development of aerodynamics to the high techwar in the future (in Chinese). In: 2003 Proceeding of Aerodynamics, Beijing, 2003. 73–80
3. Prandtl L. Uber Flussigkeitsbewegung bei sehr kleiner Reibung. In: Proceedings of the third interntional mathematics congress, Heidelberg, 1904. 484–491
4. Gad-el-Hak M, Pollard A, Bonnet J. Flow Control: Fundamentals and Practices. Berlin: Springer, 199810.1007/3-540-69672-5 ↗
5. Gad-el-Hak. Flow Control. Cambridge: Cambridge University Press, 200010.1017/CBO9780511529535 ↗
6. Collis S S, Josiln R D, Seifert A, et al. Issues in active flow control: theory, control, simulation, and experiment. Prog Aero Sci, 2004, 40: 237–28910.1016/j.paerosci.2004.06.001 ↗
7. Linda D K. Active flow control technology. ASME Paper No. FEDSM 2001-18196, 2001
8. Luo Z B, Xia Z X. Synthetic jet: a new, effect and efficient method for flow control (in Chinese). The 10th flow separation, vortex and flow control conference of China, Nanjing, 2004. 234–249
9. Greska B, Krothapalli A, Seiner J, et al. The effect of microjet injection on an F404 jet engine. AIAA 2005-3047, 200510.2514/6.2005-3047 ↗
10. Senier J, Ukeiley L, Jansen B. Aero-performance efficient noise reduction for the F404-400 engine. AIAA 2005-3048, 200510.2514/6.2005-3048 ↗
11. Shaw L L, Smith B R, Saddoughi. Full-scale flight demonstration of active control of a pod wake. AIAA 2006-3185, 200610.2514/6.2006-3185 ↗
12. Seifert A. Closed-Loop Active Flow Control Systems: Actuators. Berlin: Springer, 200710.1007/978-3-540-71439-2_6 ↗
13. Cattafesta L, Sheplak M. Actuators for active flow control. Annu Rev Fluid Mech, 2011, 43: 247–27210.1146/annurev-fluid-122109-160634 ↗
14. Lockheed-Martin. Future aircraft technology enhancement. http://www.fas.org/man/dod101/sys/ac/docs/fate.report/index.htm . 1997. 09-24
15. Luo Z B, Xia Z X, Wang L. Idea of designing novel high energy synthetic jet actuator and potential application in vectoring supersonic flow (in Chinese). The 13th flow separation, vortex and flow control conference of China, Nanjing, 2010. 65–70
16. Qu Z H, Zeng M, Liu W, et al. Hypersonic Aerodynamics (in Chi nese). Changsha: National University Defense Technology Press, 1999
17. Glezer A, Amitay M. Synthetic jets. Ann Rev Fluid Mech, 2002, 34: 503–52910.1146/annurev.fluid.34.090501.094913 ↗
18. Zhang P F, Wang J J, Feng L H. Review of zero-net-mass-flux jet and its application in separation flow control. Sci China Ser E-Tech Sci, 2008, 51: 1315–134410.1007/s11431-008-0174-x ↗
19. Luo Z B, Xia Z X. Advances in synthetic jet technology and applications in flow control (in Chinese). Adv Mech, 2005, 35: 221–234
20. Crawley E, Luis J. Use of piezoelectric actuators as elements of intelligent structures. AIAA J, 1987, 25: 1373–138510.2514/3.9792 ↗
21. Couldrick J S, Gai S, Milthorpe J, et al. Swept shock wave boundary layer interaction control with “smart” flap actuator. In: Australian International Aerospace Conference, Canberra, Australia, 200110.2514/6.2002-973 ↗
22. Jun H Y, Rediniotis O K, Lagoudas D C. Development of a fuel-powered shape memory alloy actuator system: I. Numerical analysis. Smart Mater Struct, 2007, 16: S81–S9410.1088/0964-1726/16/1/S09 ↗
23. Jun H Y, Rediniotis O K, Lagoudas D C. Development of a fuel-powered shape memory alloy actuator system: II. Fabrication and testing. Smart Mater Struct, 2007, 16: S95–S10710.1088/0964-1726/16/1/S10 ↗
24. Moreau E. Airflow control by non-thermal plasma actuators. J Phys D-Appl Phys, 2007, 40: 605–63610.1088/0022-3727/40/3/S01 ↗
25. Corke T C, Post M L, Orlov D M. SDBD plasma enhanced aerodynamics: concepts, optimization and applications. Prog Aerospace Sci, 2007, 43: 193–21710.1016/j.paerosci.2007.06.001 ↗
26. Jayaraman B, Shyy W. Modeling of dielectric barrier discharge-induced fluid dynamics and heat transfer. Prog Aerospace Sci, 2008, 44: 139–19110.1016/j.paerosci.2007.10.004 ↗
27. Corke T C, Enloe C L, Wilkinson S P. Dielectric barrier discharge plasma actuators for flow control. Ann Rev Fluid Mech, 2010, 42: 505–52910.1146/annurev-fluid-121108-145550 ↗
28. Li Y H, Liang H, Wu Y, et al. Research status of modeling and simulation technology of plasma aerodynamic actuation (in Chinese). J Air Force Eng Univ (Nat Sci Ed), 2008, 19: 1–5
29. Bletzinger P, Ganguly B N, Wie D, et al. Plasmas in high speed aerodynamics. J Phys D: Appl Phys, 2005, 38: R33–R5710.1088/0022-3727/38/4/R01 ↗
30. Shang J S, Surzhikov S T, Kimmel R, et al. Mechanisms of plasma actuators for hypersonic flow control. Prog Aerospace Sci, 2005, 41: 642–66810.1016/j.paerosci.2005.11.001 ↗
31. Samimy M, Adamovich L, Webb B, et al. Development and characterization of plasma actuators for high-speed jet control. Exp Fluids, 2004, 37: 577–58810.1007/s00348-004-0854-7 ↗
32. Grossman K R, Cybyk B Z, VanWie D M. Sparkjet actuators for flow control. AIAA 2003-57, 200310.2514/6.2003-57 ↗
33. Donovan J F, Kral L D, Cary A W. Numerical simulation of a Lorentz force actuator. AIAA 1997-1918, 199710.2514/6.1997-1918 ↗
34. Adelgren R G, Yan H, Euiott G S, et al. Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks. AIAA 2003-31, 200310.2514/6.2003-31 ↗
35. Ramachandran R, Raman G. Pulsed Shock tube actuators for noise reduction in high speed applications. AIAA 2011-1217, 201110.2514/6.2011-1217 ↗
36. Seifert A, Bachar T, Koss D, et al. Oscillatory blowing: A tool to delay boundary-layer separation. AIAA J, 1993, 31: 2052–206010.2514/3.49121 ↗
37. Seifert A, Darabi A, Wygnanski I. Delay of airfoil stall by periodic excitation. J Aircraft, 1996, 33: 691–69810.2514/3.47003 ↗
38. Honohan A, Amitay M, Glezer A. Aerodynamic control using synthetic jets. AIAA 2000-2401, 200010.2514/6.2000-2401 ↗
39. Lin J. Review of research on low-profile vortex generators to control boundary layer separation. Prog Aerospace Sci, 2002, 38: 389–42010.1016/S0376-0421(02)00010-6 ↗
40. Dolling D. Fifty years of shock-wave boundary-layer interaction research: what next? AIAA J, 2001, 30: 1517–153110.2514/2.1476 ↗
41. Selig M, Smits A. Effect of periodic blowing on attached and separated supersonic turbulent boundary layers. AIAA J, 1991, 29: 1651–165810.2514/3.10787 ↗
42. Ibrahim M, Kunimura R, Nakamura Y. Mixing enhancement of compressible jets by using unsteady microjets as actuators. AIAA J, 2002, 40: 681–68810.2514/2.1700 ↗
43. Choi J, Wee D, Alvi F. Active noise control of supersonic impinging jets using pulsed microjets. AIAA 2005-0798, 200510.2514/6.2005-2893 ↗
44. Zhuang N, Alvi F, Alkislar M, et al. Supersonic cavity flows and their control. AIAA J, 2006, 44: 2118–212810.2514/1.14879 ↗
45. Choi J, Annaswamy A, Lou H, et al. Active control of supersonic impingement tones using steady and pulsed microjets. Exp Fluids, 2006, 41: 841–85510.1007/s00348-006-0189-7 ↗
46. Bons J, River R, Sondergaard R. The fluid dynamic of LPT blade separation control using plused jets. J Turbomacb, 2002, 124: 77–8510.1115/1.1425392 ↗
47. Warsop C, Hucker M, Press A, et al. Pulsed air-jet actuators for flow separation control. Flow Turbul Combust, 2007, 78: 255–28110.1007/s10494-006-9060-4 ↗
48. Williams D, Cornelius D, Rowley C. Supersonic Cavity Response to Open-loop Forcing. Berlin: Springer, 200710.1007/978-3-540-71439-2_14 ↗
49. Raghu S. Feedback-free fluidic oscillator and method. U S Patent, 2001, No. 6253782
50. Coanda H. Device for deflecting a stream of elastic fluid projected into and elastic fluid. U S Patent, 1936, No. 2052869
51. Gregory J, Sullivan J, Raman G, et al. Characterization of the microfluidic oscillator. AIAA J, 2007, 45: 568–57610.2514/1.26127 ↗
52. Cerretelli C, Kirtley K. Boundary layer separation control with fluidic oscillators. J Turbomach, 2009, 131: 04100110.1115/1.3066242 ↗
53. Raman G, Raghu S. Cavity resonance suppression using miniature fluidic oscillators. AIAA J, 2001, 42: 2608–261110.2514/1.521 ↗
54. Gokoglu S, Kuczmarski M, Culley D, et al. Numerical studies of a supersonic fluidic diverter actuator for flow control. AIAA 2010-4415, 201010.2514/6.2010-4415 ↗
55. Solomon T, Kumar R. Alvi F. High bandwidth micro-actuators for active flow control. AIAA 2008-3042, 200810.2514/6.2008-3042 ↗
56. Solomon T, Kumar R, Alvi F. High-bandwidth pulsed microactuators for high-speed flow control. AIAA J, 2010, 48: 2386–239610.2514/1.J050405 ↗
57. Ali M, Solomon J, Gustavsson J, et al. Control of resonant flow inside a supersonic cavity using high bandwidth pulsed micro-actuators. AIAA 2010-1198, 201010.2514/6.2010-1198 ↗
58. Solomon T, Hong S, Wiley A. Control of supersonic resonant flows using high bandwidth micro-actuators. AIAA 2009-3247, 200910.2514/6.2009-3247 ↗
59. Selby G, Lin J, Howard F. Control of low-speed turbulent separated flow using jet vortex generators. Exp Fluids, 1992, 12: 394–40010.1007/BF00193886 ↗
60. Khan Z. On vortex generating jets. Int J Heat Fluid Flow, 2000, 21: 506–51110.1016/S0142-727X(00)00038-2 ↗
61. Bueno P, Wagner J, Searcy J, et al. Experiments in unsteady forcing of mach 2 shock wave/boundary layer interactions. AIAA 2006-878, 200610.2514/6.2006-878 ↗
62. Epstein A. Power MEMS and microengines. Int Conf Solid-State Sens Actuat, 1997, 2: 753–75610.1109/SENSOR.1997.635209 ↗
63. Crittenden T, Glezer A, Funk R, et al. Combustion-driven jet actuators for flow control. AIAA 2001-2768, 200110.2514/6.2001-2768 ↗
64. Crittenden T, Warta B, Glezer A. Characterization of combustion powered actuators for flow control. AIAA 2006-2864, 200610.2514/6.2006-2864 ↗
65. Rajendar A, Crittenden T, Glezer A, et al. Effect of inlet flow configuration on combustion powered actuators. AIAA 2010-1258, 201010.2514/6.2010-1258 ↗
66. Srinivasan S, Girgisy B, Menon S. Large-Eddy simulation of a combustion powered actuator. AIAA 2008-4680, 200810.2514/6.2008-4680 ↗
67. Crittenden T. Environmental testing of combustion powered actuators for flow control. AIAA 2007-3855, 200710.2514/6.2007-3855 ↗
68. Beck B, Cutler A, Drummond J, et al. A resonant pulse detonation actuator for high-speed boundary layer separation control. In: 11th International Symposium On Flow Visualization, Indiana, USA, August 9–12, 2004
69. Cutler A, Beck B, Wilkes J, et al. Development of a pulsed combustion actuator for high-speed flow control. AIAA 2005-1084, 200510.2514/6.2005-1084 ↗
70. Cutler A. High-frequency pulsed combustion actuator experiments. AIAA J, 2011, 49: 1943–195010.2514/1.J050876 ↗
71. Cutler A, Drummond J. Toward a high-frequency pulsed-detonation actuator. AIAA 2006-0635, 200610.2514/6.2006-555 ↗
72. Nguyen N, Cutler A. Pressure and thrust measurements of a high-frequency pulsed detonation tube. AIAA 2008-4690, 200810.2514/6.2008-4690 ↗
73. Raman G, Srinivasan K. The powered resonance tube: from Hartmann’s discovery to current active flow control applications. Prog Aerospace Sci, 2009, 45: 97–12310.1016/j.paerosci.2009.05.001 ↗
74. Grant N. Rapid solidification of metallic particulates. J Metals, 1983, 35: 20–26
75. Kumar A, Bushnell D, Hussaini M. Mixing augmentation technique for hypervelocity scramjets. J Prop Power, 1989, 5: 514–52210.2514/3.23184 ↗
76. Conrad E, Pavli A. A resonance tube igniter for hydrogen-oxygen rocket engines. NASA TM X-1460, 1967
77. Kadaba P, Bondarenko V, Arkharov A. Thermal characteristics of a Hartmann-Sprenger tube. Int J Refrig, 1990, 13: 309–31610.1016/0140-7007(90)90062-2 ↗
78. Raman G, Kibens V, Cain A, et al. Advanced actuator concepts for active aeroacoustic control. AIAA 2000-1930, 200010.2514/6.2000-1930 ↗
79. Raman G, Kibens V. Active flow control using integrated powered resonance tube actuators. AIAA 2001-3024, 200110.2514/6.2001-3024 ↗
80. Kastner J, Samimy M. Development and characterization of Hartmann tube fluidic actuators for high-speed flow control. AIAA J, 2002, 40: 1926–193410.2514/2.1541 ↗
81. Raman G, Sarpotdar S, Tassy J, et al. An overview of the development of high bandwidth powered resonance tube actuators: experiments and simulations. AIAA 2004-2856, 200410.2514/6.2004-2856 ↗
82. Kastner J, Hileman J, Samimy M. Exploring high-speed axisymmetric jet noise control using Hartmann tube fluidic actuators. AIAA 2004-186, 200410.2514/6.2004-186 ↗
83. Chaudhari Kedar, Sarpotdar S, Raman G. Jet noise suppression using ultrasonic powered resonance tubes. AIAA 2010-17, 201010.2514/6.2010-17 ↗
84. Cain A, Kerschen E, Tassy J, et al. Simulation of powered resonance tubes: Helmholtz resonator geometries. AIAA 2004-2690, 200410.2514/6.2004-2690 ↗
85. Raman G, Mills A, Kibens V. Development of powered resonance-tube actuators for aircraft flow control applications. J Aircraft, 2004, 41: 1306–131410.2514/1.144 ↗
86. Samimy M, Kastner J, Debiasi M. Control of high-speed impinging jets using Hartmann tube fluidic actuators. AIAA 2002-2822, 200210.2514/6.2002-2822 ↗
87. Dziuba M, Rossmann T. Active control of a sonic transverse jet in supersonic cross-flow using a powered resonance Tube. AIAA 2005-897, 200510.2514/6.2005-897 ↗
88. Seifert A, Eliahu S, Greenblatt, et al. Use of piezoelectric actuators for airfoil separation control. AIAA J, 1998, 36: 1535–153710.2514/2.549 ↗
89. Kegerise M, Cabell R, Cattafesta L. Real-time feedback control of flow-induced cavity tones, Part 1: fixed-gain control. J Sound Vib, 2007, 307: 906–92310.1016/j.jsv.2007.07.063 ↗
90. Kegerise M, Cabell R, Cattafesta L. Real-time feedback control of flow-induced cavity tones, Part 2: adaptive control. J Sound Vib, 2007, 307: 924–94010.1016/j.jsv.2007.07.062 ↗
91. Couldrick J, Gai S, Milthorpe J, et al. Active control of swept shock wave/turbulent boundary-layer interactions. Aeronaut J, 2004, 108: 93–10110.1017/S0001924000005042 ↗
92. Couldrick J, Gai S, Milthorpe J, et al. Normal shock wave/turbulent boundary-layer interaction control using ’smart’ piezoelectric actuators. Aeronaut J, 2005, 109: 577–58310.1017/S0001924000000919 ↗
93. Bandyopadhyay K. Smart materials and aerospace structures. SPIE-3903, 199910.1117/12.369472 ↗
94. Mabe J, Calkins F, Alkislar M. Variable Area Jet Nozzle Using shape memory alloy actuators in an antagonistic design. SPIE-6930, 200810.1117/12.776816 ↗
95. Travis L, Randolph H, Roberto J, et al. Testing of SMA-enabled active chevron prototypes under representative flow conditions. SPIE-6928, 200810.1117/12.776309 ↗
96. Geoff M, Leslie M, Don C, et a1. Miniature thin-film Ni-Ti hydraulic actuator with MEMS microvalves. SPIE-5762, 200510.1117/12.607307 ↗
97. Honghao T, Mohammad H. Dynamics modeling of ferromagnetic shape memory alloys (FSMA) actuators. SPIE-6173, 200610.1117/12.655629 ↗
98. Resler R, Sears W. The Prospects for magneto-aerodynamics. J Aero Sci, 1958, 25: 235–24510.2514/8.7604 ↗
99. Bletzinger P, Ganguly B, Wie D, et al. Plasma in high speed aerodynamics. J Phys D: Appl Phys, 2005, 38: R33–R5710.1088/0022-3727/38/4/R01 ↗
100. Shang J, Surzhikov S, Kimmel R, et al. Mechanisms of plasma actuators for hypersonic flow control. Prog Aerospace Sci, 2005, 41: 642–66810.1016/j.paerosci.2005.11.001 ↗