Progress and outlook of plasma-based turbulent skin-friction drag reduction

SU Zhi; ZONG Haohua; LIANG Hua; WU Yun; FANG Ziqi

doi:10.7638/kqdlxxb-2023.0083

English Version Journal Login

您当前的位置：

首页 >

文章列表页 >

Progress and outlook of plasma-based turbulent skin-friction drag reduction

更新时间：2026-05-28

- Progress and outlook of plasma-based turbulent skin-friction drag reduction
- Vol. 41, Issue 9, Pages: 1-19(2023)
- 作者机构：
  
  1. 空军工程大学航空工程学院航空动力系统与等离子体技术全国重点实验室,西安,710038
  2. 西安交通大学机械工程学院,西安,710000
  3. 西安交通大学航天航空学院,西安,710000
- 作者简介：
- 基金信息：
- DOI：10.7638/kqdlxxb-2023.0083
  CLC： P352.4;O539
- Published：2023
- 稿件说明：
移动端阅览
苏志, 宗豪华, 梁华, 等. 等离子体湍流摩擦减阻研究进展与展望[J]. 空气动力学学报, 2023, 41(9): 1−19.

SU Zhi, ZONG Haohua, LIANG Hua, et al. Progress and outlook of plasma-based turbulent skin-friction drag reduction[J]. 2023, 41(9): 1-19.
苏志, 宗豪华, 梁华, 等. 等离子体湍流摩擦减阻研究进展与展望[J]. 空气动力学学报, 2023, 41(9): 1−19. DOI： 10.7638/kqdlxxb-2023.0083

SU Zhi, ZONG Haohua, LIANG Hua, et al. Progress and outlook of plasma-based turbulent skin-friction drag reduction[J]. 2023, 41(9): 1-19. DOI： 10.7638/kqdlxxb-2023.0083.

摘要

飞机摩擦阻力可占巡航总阻力的一半以上，减小飞机湍流条件下的摩擦阻力对于提升飞机巡航性能、降低燃油消耗具有重要意义。等离子体激励是等离子体在电磁场力作用下运动或气体放电产生的压力、温度、物性变化等对气流施加的一种可控扰动。采用等离子体激励减小飞机湍流摩擦阻力具有结构重量代价小、易于智能控制等诸多优势，受到国内外广泛关注。鉴于此，按照等离子体激励特性及其与湍流边界层的相互关系，将等离子体湍流减阻方法分为非定常激励、定常激励等类型，并梳理了其研究历程与进展。在平板湍流边界层中，等离子体激励能够诱导大尺度流向涡，产生输运作用，使摩擦阻力减小40%以上；在巡航迎角工况下的翼型上，激励同样能在20 m/s的来流速度下使翼型总阻力减小13.7%。发展新型高效能、高强度等离子体激励方法，实现高雷诺数、强逆压梯度气流环境下的湍流减阻，融入机器学习，推动开环控制向智能自适应发展，是等离子体湍流减阻技术未来的发展方向。

Abstract

Aircraft friction drag accounts for more than half of the total cruising drag; thus

turbulent friction drag reduction is vital to improving flight performance and reducing flight costs. Plasma actuation is a controllable disturbance of pressure

temperature

and physical property changes caused by discharging gas or the moving plasma subjected to electromagnetic force. Compared to other turbulent friction drag reduction methods

plasma actuation has many advantages

such as lightweight and intelligent control capability

so it has received widespread attention. This paper provides a detailed overview of the development history and research progress of the plasma-based turbulent drag reduction method. In flat-plate turbulent boundary layers

plasma actuation can reduce friction drag by more than 40% by inducing large-scale vortical structures that enhance transportation. For airfoils at cruising angles of attack

plasma actuation can reduce the total drag of airfoils by up to 13.7% at a freestream velocity of 20 m/s. Developing new efficient plasma drag reduction actuation methods

adapting to flows with high Reynolds numbers and strong pressure gradients

and developing from open-loop blind control to intelligent adaptive control combining artificial intelligence

are the future development trends of the plasma-based turbulent drag reduction method.

关键词

Keywords

references

MA H D, CUI E J. Drag prediction and reduction for civil transportation aircraft[J]. Mechanics in Engineering, 2007, 29(2): 1-8. (in Chinese)

LIU P Q, ZHANG W, GUO H. Drag reduction technique for large transport aircraft[J]. Mechanics in Engineering, 2018, 40(2): 129-139, 154. . DOI: 10.6052/1000-0879-17-295(in Chinese)

THIBERT J J, RENEAUX J, SCHMITT V. ONERA activities on drag reduction[C]//17th Conference of ICAS, 1990.

GAD-EL-HAK M. Flow control: the future[J]. Journal of Aircraft, 2001, 38(3): 402-418. DOI: 10.2514/2.2796

PRANDTL L. Uber flussigkeitsbewegung bei sehr kleiner reibung[C ] //3rd International Math Congress, 1904: 484–491. https://www.damtp.cam.ac.uk/user/tong/fluids/prandtl.pdf

JOSLIN R D, MILLER D N. Fundamentals and applications of modern flow control[M]. American Institute of Aeronautics and Astronautics, 2009

LIN J C. Review of research on low-profile vortex generators to control boundary-layer separation[J]. Progress in Aerospace Sciences, 2002, 38(4-5): 389-420. DOI: 10.1016/S0376-0421(02)00010-6

GREENBLATT D, WYGNANSKI I J. The control of flow separation by periodic excitation[J]. Progress in Aerospace Sciences, 2000, 36(7): 487-545. DOI: 10.1016/s0376-0421(00)00008-7

WU Y, LI Y H. Progress and outlook of plasma flow control[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(2): 381-405. (in Chinese)

ANDERSON J D. Fundamentals of aerodynamics[M]. New York: McGraw-Hill, 2011.

ZHANG Y S, LIU D, LANG W D. Effects of geometry parameters on drag about afterbodies of transport aircraft[J]. Chinese Quarterly of Mechanics, 2013, 34(4): 585-590.

MOHSEN J. Aircraft drag reduction: an overview[R ] . Chalmers University of Technology, 2011. https://www.researchgate.net/publication/235339328_Aircraft_Drag_Reduction_An_Overview

BUSHNELL D M. Aircraft drag reduction—a review[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2003, 217(1): 1-18. DOI: 10.1243/095441003763031789

SCHUELE C Y, CORKE T C, MATLIS E. Control of stationary cross-flow modes in a Mach 3.5 boundary layer using patterned passive and active roughness[J]. Journal of Fluid Mechanics, 2013, 718: 5-38. DOI: 10.1017/jfm.2012.579

KLINE S J, REYNOLDS W C, SCHRAUB F A, et al. The structure of turbulent boundary layers[J]. Journal of Fluid Mechanics, 1967, 30(4): 741-773. DOI: 10.1017/s0022112067001740

WALSH M J. Riblets as a viscous drag reduction technique[J]. AIAA Journal, 1983, 21(4): 485-486. DOI: 10.2514/3.60126

VAN NESSELROOIJ M, VELDHUIS L M, VAN OUDHEUSDEN B W, et al. Drag reduction by means of dimpled surfaces in turbulent boundary layers[J]. Experiments in Fluids, 2016, 57(9): 142. DOI: 10.1007/s00348-016-2230-9

CHOI K S, YANG X, CLAYTON B R, et al. Turbulent drag reduction using compliant surfaces[J]. Proceedings of the Royal Society of London Series A: Mathematical, Physical and Engineering Sciences, 1997, 453(1965): 2229-2240. DOI: 10.1098/rspa.1997.0119

KIM K, SUNG H J. Effects of periodic blowing from spanwise slot on a turbulent boundary layer[J]. AIAA Journal, 2003, 41(10): 1916-1924. DOI: 10.2514/2.1907

ANTONIA R A, ZHU Y, SOKOLOV M. Effect of concentrated wall suction on a turbulent boundary layer[J]. Physics of Fluids, 1995, 7(10): 2465-2474. DOI: 10.1063/1.868690

BARON A, QUADRIO M. Turbulent drag reduction by spanwise wall oscillations[J]. Applied Scientific Research, 1995, 55(4): 311-326. DOI: 10.1007/BF00856638

CHOI K S. Near-wall structure of turbulent boundary layer with spanwise-wall oscillation[J]. Physics of Fluids, 2002, 14(7): 2530-2542. DOI: 10.1063/1.1477922

CORKE T C, ENLOE C L, WILKINSON S P. Dielectric barrier discharge plasma actuators for flow control[J]. Annual Review of Fluid Mechanics, 2010, 42: 505-529. DOI: 10.1146/annurev-fluid-121108-145550

LI Y H, WU Y, LI J. Review of the investigation on plasma flow control in China[J]. International Journal of Flow Control, 2012, 4(1-2): 1-18. DOI: 10.1260/1756-8250.4.1-2.1

POPE S B. Turbulent flows[M]. Cambridge: Cambridge University Press, 2000

XU C X. Coherent structures and drag-reduction mechanism in wall turbulence[J]. Advances in Mechanics, 2015, 45(1): 111-140. (in Chinese)

ROBINSON S K. Coherent motions in the turbulent boundary layer[J]. Annual Review of Fluid Mechanics, 1991, 23: 601-639. DOI: 10.1146/annurev.fl.23.010191.003125

CORKE T C, THOMAS F O. Active and passive turbulent boundary-layer drag reduction[J]. AIAA Journal, 2018, 56(10): 3835-3847. DOI: 10.2514/1.j056949

SOLEIMANI S, ECKELS S. A review of drag reduction and heat transfer enhancement by riblet surfaces in closed and open channel flow[J]. International Journal of Thermofluids, 2021, 9: 100053. DOI: 10.1016/j.ijft.2020.100053

WALSH M. Turbulent boundary layer drag reduction using riblets[C]//20th Aerospace Sciences Meeting, Orlando, FL, USA. Reston, Virigina: AIAA, 1982. doi: 10.2514/6.1982-169

LI S, JIANG N, YANG S Q. Influence of sinusoidal riblets on the coherent structures in turbulent boundary layer studied by time-resolved particle image velocimetry[J]. Acta Physica Sinica, 2019, 68(7): 074702.

杨绍琼. 壁湍流相干结构及其沟槽被动控制的PIV实验研究[D]. 天津: 天津大学, .

CHOI H, MOIN P, KIM J. Active turbulence control for drag reduction in wall-bounded flows[J]. Journal of Fluid Mechanics, 1994, 262: 75-110. DOI: 10.1017/s0022112094000431

HAMMOND E P, BEWLEY T R, MOIN P. Observed mechanisms for turbulence attenuation and enhancement in opposition-controlled wall-bounded flows[J]. Physics of Fluids, 1998, 10(9): 2421-2423. DOI: 10.1063/1.869759

CHUNG Y M, TALHA T. Effectiveness of active flow control for turbulent skin friction drag reduction[J]. Physics of Fluids, 2011, 23(2): 025102. DOI: 10.1063/1.3553278

FAN Y T, ZHANG Y, YE Z X, et al. Micro-blowing: effect on flow characteristics in turbulent flat plate boundary layer and drag reduction mechanism[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10): 123814(in Chinese)

TILLMAN T, HWANG D. Drag reduction on a large-scale nacelle using a micro-blowing technique[C]//37th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virigina: AIAA, 1999. doi: 10.2514/6.1999-130

HWANG D, HWANG D. A proof of concept experiment for reducing skin friction by using a micro-blowing technique[C]//35th Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virigina: AIAA, 1997. doi: 10.2514/6.1997-546

BRADSHAW P, PONTIKOS N S. Measurements in the turbulent boundary layer on an ‘infinite’ swept wing[J]. Journal of Fluid Mechanics, 1985, 159: 105. DOI: 10.1017/s0022112085003123

DRIVER D M, HEBBAR S K. Experimental study of a three-dimensional, shear-driven, turbulent boundary layer[J]. AIAA Journal, 1987, 25(1): 35-42. DOI: 10.2514/3.9575

SENDSTAD O. The near-wall mechanics of three-dimensional turbulent boundary layers[D]. Stanford, CA, USA: Stanford University, 1992.

EATON J K. Effects of mean flow three dimensionality on turbulent boundary-layer structure[J]. AIAA Journal, 1995, 33(11): 2020-2025. DOI: 10.2514/3.12942

QUADRIO M, RICCO P. Critical assessment of turbulent drag reduction through spanwise wall oscillations[J]. Journal of Fluid Mechanics, 2004, 521: 251-271. DOI: 10.1017/s0022112004001855

CHOI K S, CLAYTON B R. The mechanism of turbulent drag reduction with wall oscillation[J]. International Journal of Heat and Fluid Flow, 2001, 22(1): 1-9. DOI: 10.1016/S0142-727X(00)00070-9

KUSHAL K. Spanwise wall oscillation as a drag reduction technique[D]. Delft University of Technology, 2019.

CHIN C, ÖRLÜ R, MONTY J, et al. Simulation of a large-eddy-break-up device (LEBU) in a moderate Reynolds number turbulent boundary layer[J]. Flow, Turbulence and Combustion, 2017, 98(2): 445-460. DOI: 10.1007/s10494-016-9757-y

KIM J S, HWANG J, YOON M, et al. Influence of a large-eddy breakup device on the frictional drag in a turbulent boundary layer[J]. Physics of Fluids, 2017, 29(6): 065103. DOI: 10.1063/1.4984602

CORKE T C, GUEZENNEC Y, NAGIB H M. . Modification in drag of turbulent boundary layers resulting from manipulation of large-scale structures[R ] . NASA-CR-3444. https://ntrs.nasa.gov/api/citations/19810021850/downloads/19810021850.pdf

KLIMOV A I, KOBLOV A N, MISHIN G I, et al. Shock wave propagation in a glow discharge[J]. Technical Physics Letters, 1982, 8: 192–194.

MEYER R, PALM P, PLÖNJES E, et al. The effect of a nonequilibrium RF discharge plasma on a conical shock wave in a M = 2.5 flow[C]//32nd AIAA Plasmadynamics and Lasers Conference. doi:10.2514/6.2001-3059

LI Y H, WU Y, LIANG H, et al. Exploration and outlook of plasma-actuated gas dynamics[J]. Advances in Mechanics, 2022, 52(1): 1-32. (in Chinese)

ROTH J R, SHERMAN D M, WILKINSON S P. Electrohydrodynamic flow control with a glow-discharge surface plasma[J]. AIAA Journal, 2000, 38: 1166-1172. DOI: 10.2514/3.14531

ROTH J R, SHERMAN D M, WILKINSON S. Boundary layer flow control with a one atmosphere uniform glow discharge surface plasma[C]//36th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, USA. Reston, Virigina: AIAA, 1998. doi: 10.2514/6.1998-328

武占成, 张希军, 胡有志. 气体放电[M]. 北京: 国防工业出版社, 2012.

ROUPASSOV D V, NIKIPELOV A A, NUDNOVA M M, et al. Flow separation control by plasma actuator with nanosecond pulsed-periodic discharge[J]. AIAA Journal, 2009, 47(1): 168-185. DOI: 10.2514/1.38113

BENARD N, MOREAU E. EHD force and electric wind produced by plasma actuators used for airflow control[C]//6th AIAA Flow Control Conference, New Orleans, Louisiana, 2012. doi: 10.2514/6.2012-3136

BENARD N, MOREAU E. Electrical and mechanical characteristics of surface AC dielectric barrier discharge plasma actuators applied to airflow control[J]. Experiments in Fluids, 2014, 55(11): 1846. DOI: 10.1007/s00348-014-1846-x

ZHU Y F, WU Y, CUI W, et al. Modelling of plasma aerodynamic actuation driven by nanosecond SDBD discharge[J]. Journal of Physics D: Applied Physics, 2013, 46(35): 355205. DOI: 10.1088/0022-3727/46/35/355205

WU Y. Nanosecond pulsed discharge plasma actuation: characteristics and flow control performance[C]//45th AIAA Plasmadynamics and Lasers Conference, Atlanta, GA. Reston, Virginia: AIAA, 2014. doi: 10.2514/6.2014-2118

BENARD N, ZOUZOU N, CLAVERIE A, et al. Optical visualization and electrical characterization of fast-rising pulsed dielectric barrier discharge for airflow control applications[J]. Journal of Applied Physics, 2012, 111(3): 033303. DOI: 10.1063/1.3682568

TAKASHIMA K, ZUZEEK Y, LEMPERT W R, et al. Characterization of a surface dielectric barrier discharge plasma sustained by repetitive nanosecond pulses[J]. Plasma Sources Science and Technology, 2011, 20(5): 055009. DOI: 10.1088/0963-0252/20/5/055009

DEBIEN A, BENARD N, MOREAU E. Streamer inhibition for improving force and electric wind produced by DBD actuators[J]. Journal of Physics D: Applied Physics, 2012, 45(21): 215201. DOI: 10.1088/0022-3727/45/21/215201

LIANG H. Airfoil flow control by plasma actuation[D]. Air Force Engineering University, 2009 (in Chinese).

ZHAO G Y. Mechanism investigation of airfoil/delta wing plasma-shock-based flow control[D]. Air Force Engineering University, 2015 (in Chinese).

CUI Y D, ZHAO Z J, ZHENG J G, et al. Separation control over a NACA0015 airfoil using nanosecond pulsed plasma actuator[C]//55th AIAA Aerospace Sciences Meeting, Grapevine, Texas. Reston, Virginia: AIAA, 2017. doi: 10.2514/6.2017-0715

DURASIEWICZ C, SINGH A, LITTLE J C. A comparative flow physics study of NS-DBD vs AC-DBD plasma actuators for transient separation control on a NACA0012 airfoil[C]//2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida. Reston, Virginia: AIAA, 2018. doi: 10.2514/6.2018-1061

LIKHANSKII A, SHNEIDER M, OPAITS D, et al. Limitations of the DBD effects on the external flow[C]//48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida. Reston, Virigina: AIAA, 2010. doi: 10.2514/6.2010-470

KELLEY C L, BOWLES P O, COONEY J, et al. Leading-edge separation control using alternating-current and nanosecond-pulse plasma actuators[J]. AIAA Journal, 2014, 52(9): 1871-1884. DOI: 10.2514/1.j052708

ZHANG X, HUANG Y, YANG P Y, et al. Flight test of flow separation control using plasma UAV[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(2): 121587(in Chinese).

SU Z, LI J, LIANG H, et al. UAV flight test of plasma slats and ailerons with microsecond dielectric barrier discharge[J]. Chinese Physics B, 2018, 27(10): 105205. DOI: 10.1088/1674-1056/27/10/105205

CHOI K S, JUKES T, WHALLEY R. Turbulent boundary-layer control with plasma actuators[J]. Philosophical Transactions of the Royal Society A: Mathematical, Physical and Engineering Sciences, 2011, 369(1940): 1443-1458. DOI: 10.1098/rsta.2010.0362

CHENG X Q, WONG C W, HUSSAIN F, et al. Flat plate drag reduction using plasma-generated streamwise vortices[J]. Journal of Fluid Mechanics, 2021, 918: A24. DOI: 10.1017/jfm.2021.311

LI Y Q, GAO C, WU B, et al. Turbulent boundary layer control with a spanwise array of DBD plasma actuators[J]. Plasma Science and Technology, 2021, 23(2): 025501. DOI: 10.1088/2058-6272/abce0d

SU Z, ZONG H H, LIANG H, et al. Minimizing airfoil drag at low angles of attack with DBD-based turbulent drag reduction methods[J]. Chinese Journal of Aeronautics, 2023, 36(4): 104-119. DOI: 10.1016/j.cja.2022.11.019

SU Z. Method and mechanism investigation of flat plate/airfoil friction drag reduction by spanwise plasma actuation array[D]. Air Force Engineering University, 2022 (in Chinese).

THOMAS F O, CORKE T C, DUONG A, et al. Turbulent drag reduction using pulsed-DC plasma actuation[J]. Journal of Physics D: Applied Physics, 2019, 52(43): 434001. DOI: 10.1088/1361-6463/ab3388

YATES K, CORKE T, THOMAS F, et al. Viscous drag reduction in adverse pressure gradient boundary layers[C]//AIAA Scitech 2019 Forum, San Diego, California. Reston, Virginia: AIAA, 2019. doi: 10.2514/6.2019-0309

JUNG W J, MANGIAVACCHI N, AKHAVAN R. Suppression of turbulence in wall-bounded flows by high-frequency spanwise oscillations[J]. Physics of Fluids A: Fluid Dynamics, 1992, 4(8): 1605-1607. DOI: 10.1063/1.858381

DU Y Q, KARNIADAKIS G E. Suppressing wall turbulence by means of a transverse traveling wave[J]. Science, 2000, 288(5469): 1230. DOI: 10.1126/science.288.5469.1230

DU Y Q, SYMEONIDIS V, KARNIADAKIS G E. Drag reduction in wall-bounded turbulence via a transverse travelling wave[J]. Journal of Fluid Mechanics, 2002, 457: 1-34. DOI: 10.1017/s0022112001007613

KARNIADAKIS G E, CHOI K S. Mechanisms on transverse motions in turbulent wall flows[J]. Annual Review of Fluid Mechanics, 2003, 35: 45-62. DOI: 10.1146/annurev.fluid.35.101101.161213

WILKINSON S P. Investigation of an oscillating surface plasma for turbulent drag reduction[C ] //41st Aerospace Sciences Meeting and Exhibit, Reno, N , 2003. AIAA 2003-1023. https://ntrs.nasa.gov/api/citations/20030004240/downloads/20030004240.pdf

HEHNER M T, GATTI D, KRIEGSEIS J. Stokes-layer formation under absence of moving parts—a novel oscillatory plasma actuator design for turbulent drag reduction[J]. Physics of Fluids, 2019, 31(5): 051701. DOI: 10.1063/1.5094388

HEHNER M T, GATTI D, MATTERN P, et al. Virtual wall oscillations forced by a DBD plasma actuator operating under beat frequency - a concept for turbulent drag reduction[C]//AIAA Aviation 2020 Forum, Virtual Event. Reston, Virginia: AIAA, 2020. doi: 10.2514/6.2020-2956

JUKES T, CHOI K S, JOHNSON G, et al. Turbulent drag reduction by surface plasma through spanwise flow oscillation[C]//3rd AIAA Flow Control Conference, San Francisco, California. Reston, Virigina: AIAA, 2006. doi: 10.2514/6.2006-3693

ELAM D. A direct numerical simulation of dielectric barrier discharge (DBD) plasma actuators for turbulent skin-friction control[D]. Coventry, West Midlands, UK: University of Warwick, 2012.

SHYY W, JAYARAMAN B, ANDERSSON A. Modeling of glow discharge-induced fluid dynamics[J]. Journal of Applied Physics, 2002, 92(11): 6434-6443. DOI: 10.1063/1.1515103

ALTıNTAŞ A, DAVIDSON L, PENG S H. Direct numerical simulation of drag reduction by spanwise oscillating dielectric barrier discharge plasma force[J ] . Physics of Fluids, 2020, 32(7): 075101. doi: 10.1063/5.0007103 https://publications.lib.chalmers.se/records/fulltext/245839/local_245839.pdf

MAHFOZE O, LAIZET S. Skin-friction drag reduction in a channel flow with streamwise-aligned plasma actuators[J]. International Journal of Heat and Fluid Flow, 2017, 66: 83-94. DOI: 10.1016/j.ijheatfluidflow.2017.05.013

ALESSIO M. DNS study of turbulent drag reduction via DBD plasma actuators[D]. Politecnico di Milano, 2020.

SU Z, ZONG H H, LIANG H, et al. Optimization in frequency characteristics of an oscillating dielectric barrier discharge plasma actuator[J]. Sensors and Actuators A: Physical, 2023, 351: 114195. DOI: 10.1016/j.sna.2023.114195

WHALLEY R D, CHOI K S. The starting vortex in quiescent air induced by dielectric-barrier-discharge plasma[J]. Journal of Fluid Mechanics, 2012, 703: 192-203. DOI: 10.1017/jfm.2012.206

WHALLEY R D. Turbulent boundary-layer control with DBD plasma actuators using spanwise travelling-wave technique[D]. Nottingham, East Midlands, UK: The University of Nottingham, 2011.

WHALLEY R D, CHOI K S. Turbulent boundary-layer control with spanwise travelling waves[J]. Journal of Physics: Conference Series, 2011, 318(2): 022039. DOI: 10.1088/1742-6596/318/2/022039

WHALLEY R D, CHOI K S. Turbulent boundary-layer control with plasma spanwise travelling waves[J]. Experiments in Fluids, 2014, 55(8): 1796. DOI: 10.1007/s00348-014-1796-3

HUANG L P, CHOI K S, FAN B C. Formation of low-speed ribbons in turbulent channel flow subject to a spanwise travelling wave[J]. Journal of Physics: Conference Series, 2011, 318(2): 022027. DOI: 10.1088/1742-6596/318/2/022027

ZHAO H, WU J Z, LUO J S . Turbulent drag reduction by traveling wave of flexible wall[J]. Fluid Dynamics Research, 2004, 34(3): 175-198. DOI: 10.1016/j.fluiddyn.2003.11.001

ZONG H H, SU Z, LIANG H, et al. Experimental investigation and reduced-order modeling of plasma jets in a turbulent boundary layer for skin-friction drag reduction[J]. Physics of Fluids, 2022, 34(8): 085133. DOI: 10.1063/5.0104609

LI Y P, WONG C W, LI Y Z, et al. Drag reduction of a turbulent boundary layer using plasma actuators[C ] //19th Australasian Fluid Mechanics Conference, Melbourne, Australia, 2014. https://people.eng.unimelb.edu.au/imarusic/proceedings/19/340.pdf

WONG C W, ZHOU Y, LI Y Z, et al. Active drag reduction in a turbulent boundary layer based on plasma-actuator-generated streamwise vortices[C ] //9th International Symposium on Turbulence and Shear Flow Phenomena, Melbourne, Australia, 2015. http://www.tsfp-conference.org/proceedings/2015/v3/9A-5.pdf

彭倩. 基于等离子体激励器控制湍流边界层减阻的参数优化研究[D]. 哈尔滨: 哈尔滨工业大学, 2018.

WONG C W, X Q CHENG, Q PENG, et al. Effects of plasma-actuator-generated vortices on a turbulent boundary layer[R]. 10th International Symposium on Turbulence and Shear Flow Phenomena, Chicago, USA, 2017.

WONG C W, CHENG X Q, FAN D W, et al. Friction drag reduction based on a proportional-derivative control scheme[J]. Physics of Fluids, 2021, 33(7): 075115. DOI: 10.1063/5.0056169

ZHENG H B, GAO C, WU B, et al. Drag reduction control of turbulent boundary layer based on plasma actuation[J]. Journal of Aerospace Power, 2023, 38(5): 1157-1165. (in Chinese)

MCGOWEN R, CORKE T C, MATLIS E H, et al. Pulsed-DC plasma actuator characteristics and application in compressor stall control[C]//54th AIAA Aerospace Sciences Meeting, San Diego, California, USA. Reston, Virginia: AIAA, 2016. doi: 10.2514/6.2016-0394

MURPHY J, LAVOIE P. Characterization of DBD plasma actuators via PIV measurements[C]//51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine, Texas. Reston, Virigina: AIAA, 2013. doi: 10.2514/6.2013-346

MCGOWAN R C, CORKE T C, MATLIS E H, et al. Pulsed-DC plasma actuation for stall control in an axial fan[C]//2018 AIAA Aerospace Sciences Meeting, Kissimmee, Florida. Reston, Virginia: AIAA, 2018. doi: 10.2514/6.2018-1357

SONTAG J M, GORDEYEV S, DUONG A, et al. Studies of pulsed-DC plasma actuator and its effect on turbulent boundary layers using novel optical diagnostics[C]//AIAA Scitech 2019 Forum, San Diego, California. Reston, Virginia: AIAA, 2019. doi: 10.2514/6.2019-0468

DUONG A, MIDYA S, CORKE T C, et al. Turbulent boundary layer drag reduction using pulsed-dc plasma actuation[C]//11th International Symposium on Turbulence and Shear Flow Phenomena, Southampton, UK, 2019.

BLACKWELDER R F, KAPLAN R E. On the wall structure of the turbulent boundary layer[J]. Journal of Fluid Mechanics, 1976, 76(1): 89-112. DOI: 10.1017/s0022112076003145

DUONG A H, CORKE T C, THOMAS F O. Characteristics of drag reduced turbulent boundary layers through pulsed-DC actuation[C]//AIAA Scitech 2020 Forum, Orlando, FL. Reston, Virginia: AIAA, 2020. doi: 10.2514/6.2020-0098

DUONG A H, CORKE T C, THOMAS F O. Characteristics of drag-reduced turbulent boundary layers with pulsed-direct-current plasma actuation[J]. Journal of Fluid Mechanics, 2021, 915: A113. DOI: 10.1017/jfm.2021.167

CAIN A B, NELSON C C. Studies of the effects of drag reduction due to plasma actuation applied to aircraft configurations[C]//AIAA Scitech 2019 Forum, San Diego, California. Reston, Virginia: AIAA, 2019. doi: 10.2514/6.2019-2180

NAKAI S, NISHIDA H, OSHIO Y. Investigation on performance characteristics of dielectric discharge plasma actuator using pulsed-dc waveform[J]. Journal of Fluid Science and Technology, 2018, 13(3): JFST0018. DOI: 10.1299/jfst.2018jfst0018

STARIKOVSKIY A Y, ALEKSANDROV N L. Gasdynamic flow control by ultrafast local heating in a strongly nonequilibrium pulsed plasma[J]. Plasma Physics Reports, 2021, 47(2): 148-209. DOI: 10.1134/s1063780x21020069

SU Z, ZONG H H, LIANG H, et al. Effect of pulse width on the characteristics of a dielectric barrier discharge plasma actuator driven by high-voltage pulses[J]. Journal of Physics D: Applied Physics, 2021, 54(33): 33LT02. DOI: 10.1088/1361-6463/ac00f0

SU Z, ZONG H H, LIANG H, et al. Characteristics of a dielectric barrier discharge plasma actuator driven by pulsed-DC high voltage[J]. Journal of Physics D: Applied Physics, 2022, 55(7): 075203. DOI: 10.1088/1361-6463/ac30bc

WU B, GAO C, LIU F, et al. Reduction of turbulent boundary layer drag through dielectric-barrier-discharge plasma actuation based on the Spalding formula[J]. Plasma Science and Technology, 2019, 21(4): 045501. DOI: 10.1088/2058-6272/aaf2e2

ZONG H H, WU Y, LIANG H, et al. Experimental investigation and intelligent optimization of airfoil zero-lift drag reduction with plasma actuators[J]. AIAA Journal, 2023, 61(1): 223-240. DOI: 10.2514/1.j062099

Views

下载量

CSCD

Alert me when the article has been cited

提交

Tools

Publicity Resources

Vorticity transport characteristics of separated shear layer under AC/NS-DBD plasma actuation

Effect on near-wall region flow by an array of dielectric barrierdischarge plasma actuators

Numerical simulation of hypersonic magnetofluid control based on non-linear coupling constitutive relation

Influence of slotted track on aerodynamic characteristics of high-speed maglev train

Research status of aerodynamic design for integrated propulsion and airframe in near-space high-altitude long-endurance (HALE) UAVs

Related Author

ZHAO Guangyin

YANG Yongdong

LI Tingting

XIAO Chunhua

YAN Li

QIN Litao

ZHANG Haideng

WANG Yizhou

Related Institution

Science and Technology on Plasma Dynamics Laboratory, Air Force Engineering University, Xi'an

Collaborative Innovation Center for Advanced Aero-Engine, Beijing

School of Power and Energy, Northwestern Polytechnical University, Xi'an

Key Laboratory of Traffic Safety on the Track of Ministry of Education, Central South University, Changsha

China Railway Siyuan Survey and Design Group Co., Ltd, Wuhan

AI问答

⁰