Characteristics of pulsed plasma synthetic jet and its control effect on supersonic flow
The plasma synthetic jet is a novel flow control approach which is currently being studied. In this paper its characteristic and control effect on supersonic flow is investigated both experimentally and numerically. In the experiment, the formation of plasma synthetic jet and its propagation velocit...
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| Published in | Chinese journal of aeronautics Vol. 28; no. 1; pp. 66 - 76 |
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| Main Authors | , , , , , , |
| Format | Journal Article |
| Language | English |
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Elsevier Ltd
01.02.2015
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| Abstract | The plasma synthetic jet is a novel flow control approach which is currently being studied. In this paper its characteristic and control effect on supersonic flow is investigated both experimentally and numerically. In the experiment, the formation of plasma synthetic jet and its propagation velocity in quiescent air are recorded and calculated with time resolved schlieren method. The jet velocity is up to 100 m/s and no remarkable difference has been found after changing discharge parameters. When applied in Mach 2 supersonic flow, an obvious shockwave can be observed. In the modeling of electrical heating, the arc domain is not defined as an initial condition with fixed temperature or pressure, but a source term with time-varying input power density, which is expected to better describe the influence of heating process. Velocity variation with different heating efficiencies is presented and discussed and a peak velocity of 850 m/s is achieved in still air with heating power density of 5.0 · 1012W/m3. For more details on the interaction between plasma synthetic jet and supersonic flow, the plasma synthetic jet induced shockwave and the disturbances in the boundary layer are numerically researched. All the results have demonstrated the control authority of plasma synthetic jet onto supersonic flow. |
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| AbstractList | The plasma synthetic jet is a novel flow control approach which is currently being studied. In this paper its characteristic and control effect on supersonic flow is investigated both experimentally and numerically. In the experiment, the formation of plasma synthetic jet and its propagation velocity in quiescent air are recorded and calculated with time resolved schlieren method. The jet velocity is up to 100m/s and no remarkable difference has been found after changing discharge parameters. When applied in Mach 2 supersonic flow, an obvious shockwave can be observed. In the modeling of electrical heating, the arc domain is not defined as an initial condition with fixed temperature or pressure, but a source term with time-varying input power density, which is expected to better describe the influence of heating process. Velocity variation with different heating efficiencies is presented and discussed and a peak velocity of 850m/s is achieved in still air with heating power density of 5.0×1012W/m3. For more details on the interaction between plasma synthetic jet and supersonic flow, the plasma synthetic jet induced shockwave and the disturbances in the boundary layer are numerically researched. All the results have demonstrated the control authority of plasma synthetic jet onto supersonic flow. The plasma synthetic jet is a novel flow control approach which is currently being studied. In this paper its characteristic and control effect on supersonic flow is investigated both experimentally and numerically. In the experiment, the formation of plasma synthetic jet and its propagation velocity in quiescent air are recorded and calculated with time resolved schlieren method. The jet velocity is up to 100 m/s and no remarkable difference has been found after changing discharge parameters. When applied in Mach 2 supersonic flow, an obvious shockwave can be observed. In the modeling of electrical heating, the are domain is not defined as an initial condition with fixed temperature or pressure, but a source term with time-varying input power density, which is expected to better describe the influence of heating process. Velocity variation with different heating efficiencies is presented and discussed and a peak velocity of 850 m/s is achieved in still air with heating power density of 5.0 x 10 super(12) W/m super(3). For more details on the interaction between plasma synthetic jet and supersonic flow, the plasma synthetic jet induced shockwave and the disturbances in the boundary layer are numerically researched. All the results have demonstrated the control authority of plasma synthetic jet onto supersonic flow. The plasma synthetic jet is a novel flow control approach which is currently being studied. In this paper its characteristic and control effect on supersonic flow is investigated both experimentally and numerically. In the experiment, the formation of plasma synthetic jet and its propagation velocity in quiescent air are recorded and calculated with time resolved schlieren method. The jet velocity is up to 100 m/s and no remarkable difference has been found after changing discharge parameters. When applied in Mach 2 supersonic flow, an obvious shockwave can be observed. In the modeling of electrical heating, the arc domain is not defined as an initial condition with fixed temperature or pressure, but a source term with time-varying input power density, which is expected to better describe the influence of heating process. Velocity variation with different heating efficiencies is presented and discussed and a peak velocity of 850 m/s is achieved in still air with heating power density of 5.0 · 1012W/m3. For more details on the interaction between plasma synthetic jet and supersonic flow, the plasma synthetic jet induced shockwave and the disturbances in the boundary layer are numerically researched. All the results have demonstrated the control authority of plasma synthetic jet onto supersonic flow. |
| Author | Jin Di Cui Wei Li Yinghong Li Fanyu Jia Min Sun Quan Zhang Bailing |
| AuthorAffiliation | Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi＇an 710038, China School of Aerospace Engineering, Tsinghua University, Beijing 100084, China |
| Author_xml | – sequence: 1 givenname: Di surname: Jin fullname: Jin, Di email: james.8653@gmail.com organization: Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China – sequence: 2 givenname: Wei surname: Cui fullname: Cui, Wei email: cw14@mails.tsinghua.edu.cn organization: School of Aerospace Engineering, Tsinghua University, Beijing 100084, China – sequence: 3 givenname: Yinghong surname: Li fullname: Li, Yinghong organization: Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China – sequence: 4 givenname: Fanyu surname: Li fullname: Li, Fanyu organization: Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China – sequence: 5 givenname: Min surname: Jia fullname: Jia, Min organization: Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China – sequence: 6 givenname: Quan surname: Sun fullname: Sun, Quan organization: Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China – sequence: 7 givenname: Bailing surname: Zhang fullname: Zhang, Bailing organization: Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi’an 710038, China |
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| Cites_doi | 10.1063/1.869718 10.1088/0964-1726/17/01/015013 10.2514/1.J052686 10.2514/6.2003-57 10.2514/6.2008-285 10.2514/6.1998-208 10.2514/1.41352 10.1063/1.4731292 10.2514/6.2004-2131 10.2514/6.2003-3711 10.1016/S1000-9361(09)60249-1 10.2514/1.J052022 10.2514/1.J051309 10.1088/1009-0630/15/10/14 10.1088/0022-3727/44/36/365201 10.2514/6.2010-5103 10.2514/6.2004-2689 10.2514/1.J051246 10.1063/1.869828 10.2514/6.2010-1089 10.2514/6.1998-209 10.2514/6.2010-4979 10.2514/6.2009-1307 10.2514/6.2008-3759 10.2514/6.2006-478 10.7498/aps.62.125207 |
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| Keywords | Supersonic flow Shockwave Plasma aerodynamic actuation Synthetic jet Pulsed direct current (DC) discharge |
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| Notes | supersonic heating shockwave authority actuator details currently pulsed numerically remarkable The plasma synthetic jet is a novel flow control approach which is currently being studied. In this paper its characteristic and control effect on supersonic flow is investigated both experimentally and numerically. In the experiment, the formation of plasma synthetic jet and its propagation velocity in quiescent air are recorded and calculated with time resolved schlieren method. The jet velocity is up to 100 m/s and no remarkable difference has been found after changing discharge parameters. When applied in Mach 2 supersonic flow, an obvious shockwave can be observed. In the modeling of electrical heating, the arc domain is not defined as an initial condition with fixed temperature or pressure, but a source term with time-varying input power density, which is expected to better describe the influence of heating process. Velocity variation with different heating efficiencies is presented and discussed and a peak velocity of 850 m/s is achieved in still air with heating power density of 5.0 · 1012W/m3. For more details on the interaction between plasma synthetic jet and supersonic flow, the plasma synthetic jet induced shockwave and the disturbances in the boundary layer are numerically researched. All the results have demonstrated the control authority of plasma synthetic jet onto supersonic flow. 11-1732/V ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
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| References | Narayanaswamy, Raja, Clemens (b0070) 2010; 48 2003 Jan 6–9; Reno, Nevada. Reston: AIAA; 2003. 2006 Jan 9–12; Reno, Nevada. Reston: AIAA; 2006. 2008 Jan 7–10; Reno, Nevada. Reston: AIAA; 2008. Belinger, Hardy, Barricau, Cambronne, Caruana (b0105) 2011; 44 Narayanaswamy, Raja, Clemens (b0075) 2012; 50 2004 Jun 28–Jul 1; Portland, Oregon. Reston: AIAA; 2004. Cybyk BZ, Wilkerson JT, Grossman KR. Performance characteristics of the sparkjet flow control actuator. Haack SJ, Land HB, Cybyk BZ, Ko HS, Katz J. Characterization of a high-speed flow control actuator using digital speckle tomography and PIV. Jin, Li, Jia, Song, Cui, Sun (b0135) 2013; 15 Wang, Luo, Xia, Liu (b0125) 2013; 62 Wang, Xia, Luo, Chen (b0130) 2014; 52 Smith, Amitay, Kibens, Parekh, Glezer (b0030) 1998 Cybyk BZ, Simon DH, Land HB, Chen J, Katz J. Experimental characterization of a supersonic flow control actuator. 2008 Jun 23–26; Seattle, Washington. Reston: AIAA; 2008. Shin (b0100) 2010; 23 Mane, Mossi, Bryant (b0015) 2008; 17 Cybyk BZ, Wilkerson JT, Grossman KR, VanWei DM. Computational assessment of the sparkjet flow control actuator. Haack SJ, Taylor T, Emhoff J, Cybyk BZ. Development of an analytical sparkjet model. Smith, Glezer (b0005) 1998; 10 2003 Jun 23–26; Orlando, Florida. Reston: AIAA; 2003. Narayanaswamy V, Shin J, Clemens NT, Raja LL. Investigation of plasma-generated jets for supersonic flow control. Wiltse, Glezer (b0020) 1998; 10 Narayanaswamy, Raja, Clemens (b0085) 2012; 24 Anderson, Knight (b0120) 2012; 50 Reedy, Kale, Dutton, Elliott (b0095) 2013; 51 Caruana D, Barricau P, Hardy P, Cambronne JP, Belinger A. The plasma synthetic jet actuator. Aero-thermodynamic characterization and first flow control applications. 2010 Jun 28–Jul 1; Chicago, Illinois. Reston: AIAA; 2010. Amitay, Smith, Glezer (b0025) 1998 2009 Jan 5–8; Orlando, Florida. Reston: AIAA; 2009. Glezer (b0010) 1940; 2011 2010 Jan 4–7; Orlando, Florida. Reston: AIAA; 2010. Crittenden TM, Shlyubsky D, Glezer A. Combustion-driven jet actuators in reversed flow configurations. Grossman KR, Cybyk BZ, van Wei DM. Sparkjet actuators for flow control. Narayanaswamy V, Clemens NT, Raja LL. Investigation of a pulsed-plasma jet for shock/boundary layer control. Hardy P, Barricau P, Belinger A, Caruana D, Cambronne JP, Gleyzes C. Plasma synthetic jet for flow control. Narayanaswamy (10.1016/j.cja.2014.12.012_b0075) 2012; 50 Anderson (10.1016/j.cja.2014.12.012_b0120) 2012; 50 Mane (10.1016/j.cja.2014.12.012_b0015) 2008; 17 Amitay (10.1016/j.cja.2014.12.012_b0025) 1998 Narayanaswamy (10.1016/j.cja.2014.12.012_b0070) 2010; 48 Smith (10.1016/j.cja.2014.12.012_b0005) 1998; 10 10.1016/j.cja.2014.12.012_b0155 10.1016/j.cja.2014.12.012_b0140 10.1016/j.cja.2014.12.012_b0185 Glezer (10.1016/j.cja.2014.12.012_b0010) 1940; 2011 10.1016/j.cja.2014.12.012_b0180 Smith (10.1016/j.cja.2014.12.012_b0030) 1998 10.1016/j.cja.2014.12.012_b0160 Belinger (10.1016/j.cja.2014.12.012_b0105) 2011; 44 Wiltse (10.1016/j.cja.2014.12.012_b0020) 1998; 10 Wang (10.1016/j.cja.2014.12.012_b0125) 2013; 62 Shin (10.1016/j.cja.2014.12.012_b0100) 2010; 23 10.1016/j.cja.2014.12.012_b0165 10.1016/j.cja.2014.12.012_b0145 10.1016/j.cja.2014.12.012_b0150 Wang (10.1016/j.cja.2014.12.012_b0130) 2014; 52 Narayanaswamy (10.1016/j.cja.2014.12.012_b0085) 2012; 24 10.1016/j.cja.2014.12.012_b0175 10.1016/j.cja.2014.12.012_b0190 Jin (10.1016/j.cja.2014.12.012_b0135) 2013; 15 10.1016/j.cja.2014.12.012_b0170 Reedy (10.1016/j.cja.2014.12.012_b0095) 2013; 51 |
| References_xml | – volume: 23 start-page: 518 year: 2010 end-page: 522 ident: b0100 article-title: Characteristics of high speed electron-thermal jet activated by pulsed DC discharge publication-title: Chin J Aeronaut contributor: fullname: Shin – volume: 24 start-page: 076101 year: 2012 ident: b0085 article-title: Control of unsteadiness of a shock wave/turbulent boundary layer interaction by using a pulsed-plasma-jet actuator publication-title: Phys Fluids contributor: fullname: Clemens – volume: 62 start-page: 125207 year: 2013 ident: b0125 article-title: Energy efficiency and performance characteristics of plasma synthetic jet publication-title: Acta Phys Sin contributor: fullname: Liu – volume: 17 start-page: 015013 year: 2008 ident: b0015 article-title: Experimental design and analysis for piezoelectric circular actuators in flow control application publication-title: Smart Mater Struct contributor: fullname: Bryant – volume: 10 start-page: 2026 year: 1998 end-page: 2036 ident: b0020 article-title: Direct excitation of small-scale motions in free shear flows publication-title: Phys Fluids contributor: fullname: Glezer – volume: 10 start-page: 2281 year: 1998 end-page: 2297 ident: b0005 article-title: The formation and evolution of synthetic jets publication-title: Phys Fluids contributor: fullname: Glezer – volume: 50 start-page: 246 year: 2012 end-page: 249 ident: b0075 article-title: Control of a shock/boundary-layer interaction by using a pulsed-plasma jet actuator publication-title: AIAA J contributor: fullname: Clemens – volume: 15 start-page: 1034 year: 2013 end-page: 1040 ident: b0135 article-title: Experimental characterization of the plasma synthetic jet actuator publication-title: Plasma Sci Technol contributor: fullname: Sun – volume: 52 start-page: 879 year: 2014 end-page: 882 ident: b0130 article-title: Three-electrode plasma synthetic jet actuator for high-speed flow control publication-title: AIAA J contributor: fullname: Chen – volume: 2011 start-page: 1476 year: 1940 end-page: 1494 ident: b0010 article-title: Some aspects of aerodynamic flow control using synthetic-jet actuation publication-title: Philos Trans R Soc A contributor: fullname: Glezer – volume: 50 start-page: 1855 year: 2012 end-page: 1872 ident: b0120 article-title: Plasma jet for flow control publication-title: AIAA J contributor: fullname: Knight – volume: 48 start-page: 297 year: 2010 end-page: 305 ident: b0070 article-title: Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control publication-title: AIAA J contributor: fullname: Clemens – volume: 44 start-page: 365201 year: 2011 ident: b0105 article-title: Influence of the energy dissipation rate in the discharge of a plasma synthetic jet actuator publication-title: J Phys D Appl Phys contributor: fullname: Caruana – year: 1998 ident: b0030 article-title: Modification of lifting body aerodynamics using synthetic jet actuators publication-title: Proceedings of 36th Aerospace Sciences Meeting and Exhibit contributor: fullname: Glezer – year: 1998 ident: b0025 article-title: Aerodynamic flow control using synthetic jet technology publication-title: Proceedings of 36th Aerospace Sciences Meeting and Exhibit contributor: fullname: Glezer – volume: 51 start-page: 2027 year: 2013 end-page: 2031 ident: b0095 article-title: Experimental characterization of a pulsed plasma jet publication-title: AIAA J contributor: fullname: Elliott – volume: 10 start-page: 2026 issue: 8 year: 1998 ident: 10.1016/j.cja.2014.12.012_b0020 article-title: Direct excitation of small-scale motions in free shear flows publication-title: Phys Fluids doi: 10.1063/1.869718 contributor: fullname: Wiltse – volume: 17 start-page: 015013 issue: 1 year: 2008 ident: 10.1016/j.cja.2014.12.012_b0015 article-title: Experimental design and analysis for piezoelectric circular actuators in flow control application publication-title: Smart Mater Struct doi: 10.1088/0964-1726/17/01/015013 contributor: fullname: Mane – volume: 52 start-page: 879 issue: 4 year: 2014 ident: 10.1016/j.cja.2014.12.012_b0130 article-title: Three-electrode plasma synthetic jet actuator for high-speed flow control publication-title: AIAA J doi: 10.2514/1.J052686 contributor: fullname: Wang – ident: 10.1016/j.cja.2014.12.012_b0145 doi: 10.2514/6.2003-57 – ident: 10.1016/j.cja.2014.12.012_b0175 doi: 10.2514/6.2008-285 – year: 1998 ident: 10.1016/j.cja.2014.12.012_b0025 article-title: Aerodynamic flow control using synthetic jet technology doi: 10.2514/6.1998-208 contributor: fullname: Amitay – volume: 48 start-page: 297 issue: 2 year: 2010 ident: 10.1016/j.cja.2014.12.012_b0070 article-title: Characterization of a high-frequency pulsed-plasma jet actuator for supersonic flow control publication-title: AIAA J doi: 10.2514/1.41352 contributor: fullname: Narayanaswamy – volume: 24 start-page: 076101 issue: 7 year: 2012 ident: 10.1016/j.cja.2014.12.012_b0085 article-title: Control of unsteadiness of a shock wave/turbulent boundary layer interaction by using a pulsed-plasma-jet actuator publication-title: Phys Fluids doi: 10.1063/1.4731292 contributor: fullname: Narayanaswamy – ident: 10.1016/j.cja.2014.12.012_b0155 doi: 10.2514/6.2004-2131 – ident: 10.1016/j.cja.2014.12.012_b0150 doi: 10.2514/6.2003-3711 – volume: 23 start-page: 518 issue: 5 year: 2010 ident: 10.1016/j.cja.2014.12.012_b0100 article-title: Characteristics of high speed electron-thermal jet activated by pulsed DC discharge publication-title: Chin J Aeronaut doi: 10.1016/S1000-9361(09)60249-1 contributor: fullname: Shin – volume: 51 start-page: 2027 issue: 8 year: 2013 ident: 10.1016/j.cja.2014.12.012_b0095 article-title: Experimental characterization of a pulsed plasma jet publication-title: AIAA J doi: 10.2514/1.J052022 contributor: fullname: Reedy – volume: 50 start-page: 1855 issue: 9 year: 2012 ident: 10.1016/j.cja.2014.12.012_b0120 article-title: Plasma jet for flow control publication-title: AIAA J doi: 10.2514/1.J051309 contributor: fullname: Anderson – volume: 15 start-page: 1034 issue: 10 year: 2013 ident: 10.1016/j.cja.2014.12.012_b0135 article-title: Experimental characterization of the plasma synthetic jet actuator publication-title: Plasma Sci Technol doi: 10.1088/1009-0630/15/10/14 contributor: fullname: Jin – volume: 44 start-page: 365201 issue: 36 year: 2011 ident: 10.1016/j.cja.2014.12.012_b0105 article-title: Influence of the energy dissipation rate in the discharge of a plasma synthetic jet actuator publication-title: J Phys D Appl Phys doi: 10.1088/0022-3727/44/36/365201 contributor: fullname: Belinger – ident: 10.1016/j.cja.2014.12.012_b0190 doi: 10.2514/6.2010-5103 – ident: 10.1016/j.cja.2014.12.012_b0140 doi: 10.2514/6.2004-2689 – volume: 50 start-page: 246 issue: 1 year: 2012 ident: 10.1016/j.cja.2014.12.012_b0075 article-title: Control of a shock/boundary-layer interaction by using a pulsed-plasma jet actuator publication-title: AIAA J doi: 10.2514/1.J051246 contributor: fullname: Narayanaswamy – volume: 10 start-page: 2281 issue: 9 year: 1998 ident: 10.1016/j.cja.2014.12.012_b0005 article-title: The formation and evolution of synthetic jets publication-title: Phys Fluids doi: 10.1063/1.869828 contributor: fullname: Smith – volume: 2011 start-page: 1476 issue: 369 year: 1940 ident: 10.1016/j.cja.2014.12.012_b0010 article-title: Some aspects of aerodynamic flow control using synthetic-jet actuation publication-title: Philos Trans R Soc A contributor: fullname: Glezer – ident: 10.1016/j.cja.2014.12.012_b0180 doi: 10.2514/6.2010-1089 – year: 1998 ident: 10.1016/j.cja.2014.12.012_b0030 article-title: Modification of lifting body aerodynamics using synthetic jet actuators doi: 10.2514/6.1998-209 contributor: fullname: Smith – ident: 10.1016/j.cja.2014.12.012_b0160 doi: 10.2514/6.2010-4979 – ident: 10.1016/j.cja.2014.12.012_b0185 doi: 10.2514/6.2009-1307 – ident: 10.1016/j.cja.2014.12.012_b0170 doi: 10.2514/6.2008-3759 – ident: 10.1016/j.cja.2014.12.012_b0165 doi: 10.2514/6.2006-478 – volume: 62 start-page: 125207 issue: 12 year: 2013 ident: 10.1016/j.cja.2014.12.012_b0125 article-title: Energy efficiency and performance characteristics of plasma synthetic jet publication-title: Acta Phys Sin doi: 10.7498/aps.62.125207 contributor: fullname: Wang |
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| SubjectTerms | Density Disturbances Electric power generation Heating Mathematical models Plasma aerodynamic actuation Pulsed direct current (DC) discharge Shock waves Shockwave Supersonic aircraft Supersonic flow Synthetic jet 传播速度 功率密度 合成射流 控制效果 数值研究 时间分辨 脉冲等离子体 超音速流动 |
| Title | Characteristics of pulsed plasma synthetic jet and its control effect on supersonic flow |
| URI | http://lib.cqvip.com/qk/83889X/201501/664053233.html https://dx.doi.org/10.1016/j.cja.2014.12.012 https://search.proquest.com/docview/1709761341 |
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