Acta Aeronautica et Astronautica Sinica ›› 2023, Vol. 44 ›› Issue (15): 529002-529002.doi: 10.7527/S1000-6893.2023.29002
• Reviews • Previous Articles Next Articles
Zhenbing LUO(), Wei XIE, Xuzhen XIE, Yan ZHOU, Qiang LIU
Received:
2023-05-15
Revised:
2023-05-29
Accepted:
2023-06-19
Online:
2023-08-15
Published:
2023-06-21
Contact:
Zhenbing LUO
E-mail:luozhenbing@163.com
Supported by:
CLC Number:
Zhenbing LUO, Wei XIE, Xuzhen XIE, Yan ZHOU, Qiang LIU. Research progress of active flow control of shock wave and its interaction[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(15): 529002-529002.
Table 1
Summary and comparison of three types of active flow control technologies
控制方式 | 优点 | 缺点 | 应用对象 | 典型研究 | |
---|---|---|---|---|---|
作者 | 年份 | ||||
主动射流 | 产生方式简单,形式多样,可调节性强,可以产生不同压比,不同温度的定常/脉冲射流 | 需消耗大量气源 | 激波控制 | Finley[ Sharma和Nair[ 王泽江等[ | 1966 2020 2020 |
激波/激波干扰控制 | Prabhu等[ Albertson和Venkat[ 李帅等[ | 1991 2005 2023 | |||
激波/边界层干扰控制 | Verma和Manisankar[ 黄伟等[ 罗振兵等[ | 2012 2022 2023 | |||
激光能量沉积 | 无须开孔或改变飞行器型面,可调节性强 | 耗能高,系统复杂,局部能量沉积可能使热流上升 | 激波控制 | 王殿恺等[ 韩路阳等[ | 2018 2022 |
激波/激波干扰控制 | Adelgren等[ 王殿恺等[ | 2003-2005 2015 | |||
等离子体放电 | 无机械活动部件,结构简单,激励频带宽,响应快,适应性强 | 激励频率和输入能量存在矛盾,放电存在一定的电磁干扰 | 激波控制 | 王健等[ 周岩等[ | 2009 2019 |
激波/激波干扰控制 | 谢玮等[ 唐孟潇等[ 孔亚康等[ 张传标等[ | 2021 2022 2022 2022 | |||
激波/边界层干扰控制 | 严红和王松[ 马正雪[ 杨鹤森等[ | 2014 2022 2022 |
1 | 吴子牛, 白晨媛, 李娟, 等. 高超声速飞行器流动特征分析[J]. 航空学报, 2015, 36(1): 58-85. |
WU Z N, BAI C Y, LI J, et al. Analysis of flow characteristics for hypersonic vehicle[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(1): 58-85 (in Chinese). | |
2 | HORNUNG H. Regular and Mach reflection of shock waves[J]. Annual Review of Fluid Mechanics, 1986, 18: 33-58. |
3 | BERTIN J J, CUMMINGS R M. Fifty years of hypersonics: Where we’ve been, where we’re going[J]. Progress in Aerospace Sciences, 2003, 39(6-7): 511-536. |
4 | 杨基明, 李祝飞, 朱雨建. 高超声速流动中的激波及相互作用[M]. 北京: 国防工业出版社, 2019. |
YANG J M, LI Z F, ZHU Y J. Shock waves and shock interactions in hypersonic flow[M]. Beijing: National Defense Industry Press, 2019 (in Chinese). | |
5 | BABINSKY H, HARVEY J. Shock wave-boundary-layer interactions[M]. Cambridge: Cambridge University Press, 2011. |
6 | GAITONDE D V, ADLER M C. Dynamics of three-dimensional shock-wave/boundary-layer interactions[J]. Annual Review of Fluid Mechanics, 2023, 55: 291-321. |
7 | GAITONDE D V. Progress in shock wave/boundary layer interactions[J]. Progress in Aerospace Sciences, 2015, 72: 80-99. |
8 | WATTS J D. Flight experience with shock impingement and interference heating on the X-15-2 research airplane: NASA TMX-1669[R]. Washington, D.C.:NASA, 1968. |
9 | 周岩. 新型等离子体合成射流及其激波控制特性研究[D]. 长沙: 国防科技大学, 2018. |
ZHOU Y. Novel plasma synthetic jet and its application in shock wave control[D]. Changsha: National University of Defense Technology, 2018 (in Chinese). | |
10 | 罗振兵, 夏智勋, 王林. 高超声速飞行器内外流主动流动控制[M]. 北京: 科学出版社, 2019: 3-38. |
LUO Z B, XIA Z X, WANG L. Active flow control of internal and external flow in hypersonic vehicle[M]. Beijing: Science Press, 2019: 3-38 (in Chinese). | |
11 | 黄杰, 姚卫星. 高超声速飞行器激波控制减阻技术[J]. 宇航学报, 2020, 41(10): 1280-1287. |
HUANG J, YAO W X. Drag reduction of hypersonic vehicles by shock control[J]. Journal of Astronautics, 2020, 41(10): 1280-1287 (in Chinese). | |
12 | 陈加政, 胡国暾, 樊国超, 等. 等离子体合成射流对钝头激波的控制与减阻[J]. 航空学报, 2021, 42(7): 124773. |
CHEN J Z, HU G, FAN G C, et al. Bow shock wave control and drag reduction by plasma synthetic jet[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(7): 124773 (in Chinese). | |
13 | HUANG W, CHEN Z, YAN L, et al. Drag and heat flux reduction mechanism induced by the spike and its combinations in supersonic flows: A review[J]. Progress in Aerospace Sciences, 2019, 105: 31-39. |
14 | DURNA A S, HAJJ ALI BARADA M EL, CELIK B. Shock interaction mechanisms on a double wedge at Mach 7[J]. Physics of Fluids, 2016, 28(9): 096101. |
15 | HASHIMOTO T. Experimental investigation of hypersonic flow induced separation over double wedges[J]. Journal of Thermal Science, 2009, 18(3): 220-225. |
16 | SHIROSHANA T, VLADIMIR T, DIMITRIS D. Chemically reacting flows around a double-cone, including ablation effects[C]∥ 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. Reston: AIAA, 2010. |
17 | 李素循, 马继魁, 郭孝国. 大后掠钝舵高超声速干扰特性实验研究[J]. 气体物理, 2016, 1(3): 1-5. |
LI S X, MA J K, GUO X G. Experimental study of hypersonic interaction flow induced by high sweep fin model[J]. Physics of Gases, 2016, 1(3): 1-5 (in Chinese). | |
18 | XIANG G X, WANG C, TENG H H, et al. Investigations of three-dimensional shock/shock interactions over symmetrical intersecting wedges[J]. AIAA Journal, 2016, 54(5): 1472-1481. |
19 | EDNEY B. Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of an impinging shock: FFA-115[R]. Washington, D.C.: National Security Agency, 1968. |
20 | VAN WIE D M. Scramjet inlets: Volume 189[M]. Reston: AIAA, 2000: 447-511. |
21 | 杨基明, 李祝飞, 朱雨建, 等. 激波的传播与干扰[J]. 力学进展, 2016, 46(1): 541-587. |
YANG J M, LI Z F, ZHU Y J, et al. Shock wave propagation and interactions[J]. Advances in Mechanics, 2016, 46(1): 541-587 (in Chinese). | |
22 | MAHAPATRA D, JAGADEESH G. Studies on unsteady shock interactions near a generic scramjet inlet[J]. AIAA Journal, 2009, 47(9): 2223-2232. |
23 | ZHONG X L. Application of essentially nonoscillatory schemes to unsteady hypersonic shock-shock interference heating problems[J]. AIAA Journal, 1994, 32(8): 1606-1616. |
24 | HUANG W, WU H, YANG Y G, et al. Recent advances in the shock wave/boundary layer interaction and its control in internal and external flows[J]. Acta Astronautica, 2020, 174: 103-122. |
25 | CHANG E W K, CHAN W Y K, MCINTYRE T J, et al. Hypersonic shock impingement studies on a flat plate: Flow separation of laminar boundary layers[J]. Journal of Fluid Mechanics, 2022, 951: A19. |
26 | CLEMENS N T, NARAYANASWAMY V. Low-frequency unsteadiness of shock wave/turbulent boundary layer interactions[J]. Annual Review of Fluid Mechanics, 2014, 46: 469-492. |
27 | BUSHNELL D M. Shock wave drag reduction[J]. Annual Review of Fluid Mechanics, 2004, 36: 81-96. |
28 | SHARMA K, NAIR M T. Combination of counterflow jet and cavity for heat flux and drag reduction[J]. Physics of Fluids, 2020, 32(5): 056107. |
29 | FINLEY P J. The flow of a jet from a body opposing a supersonic free stream[J]. Journal of Fluid Mechanics, 1966, 26(2): 337-368. |
30 | 王泽江, 李杰, 曾学军, 等. 逆向喷流对双锥导弹外形减阻特性的影响[J]. 航空学报, 2020, 41(12): 124116. |
WANG Z J, LI J, ZENG X J, et al. Effect of opposing jet on drag reduction characteristics of double-cone missile shape[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(12): 124116 (in Chinese). | |
31 | 王殿恺, 文明, 王伟东, 等. 脉冲激光与正激波相互作用过程和减阻机理的实验研究[J]. 力学学报, 2018, 50(6): 1337-1345. |
WANG D K, WEN M, WANG W D, et al. Experimental study on process and mechanisms of wave drag reduction during pulsed laser interacting with normal shock[J]. Chinese Journal of Theoretical and Applied Mechanics, 2018, 50(6): 1337-1345 (in Chinese). | |
32 | 韩路阳, 王斌, 蒲亮, 等. 能量沉积减阻技术机理及相关问题研究进展[J]. 航空学报, 2022, 43(9): 026032. |
HAN L Y, WANG B, PU L, et al. Research progress on mechanism and related problems of energy deposition drag reduction technology[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(9): 026032 (in Chinese). | |
33 | 石继林, 王殿恺. 激光减阻机理研究进展[J]. 激光与红外, 2021, 51(7): 827-835. |
SHI J L, WANG D K. Research progress of laser drag reduction mechanism[J]. Laser & Infrared, 2021, 51(7): 827-835 (in Chinese). | |
34 | XIE W, LUO Z B, ZHOU Y, et al. Experimental and numerical investigation on opposing plasma synthetic jet for drag reduction[J]. Chinese Journal of Aeronautics, 2022, 35(8): 75-91. |
35 | XIE W, LUO Z B, HOU L, et al. Characterization of plasma synthetic jet actuator with Laval-shaped exit and application to drag reduction in supersonic flow[J]. Physics of Fluids, 2021, 33(9): 096104. |
36 | XIE W, LUO Z B, ZHOU Y, et al. Experimental study on plasma synthetic jet for drag reduction in hypersonic flow[J]. AIAA Journal, 2023, 61(3): 1428-1434. |
37 | LEONOV S, YARANTSEV D, SOLOVIEV V. Experiments on control of supersonic flow structure in model inlet by electrical discharge[C]∥ Proceedings of the 38th Plasmadynamics and Lasers Conference. Reston: AIAA, 2007. |
38 | LEONOV S B, YARANTSEV D A. Near-surface electrical discharge in supersonic airflow: Properties and flow control[J]. Journal of Propulsion and Power, 2008, 24(6): 1168-1181. |
39 | 王健, 李应红, 程邦勤, 等. 等离子体气动激励控制激波的机理研究[J]. 物理学报, 2009, 58(8): 5513-5519. |
WANG J, LI Y H, CHENG B Q, et al. The mechanism investigation on shock wave controlled by plasma aerodynamic actuation[J]. Acta Physica Sinica, 2009, 58(8): 5513-5519 (in Chinese). | |
40 | 王健, 李应红, 程邦勤, 等. 等离子体气动激励控制激波的实验研究[J]. 航空学报, 2009, 30(8): 1374-1379. |
WANG J, LI Y H, CHENG B Q, et al. Experimental investigation on shock wave control by plasma aerodynamic actuation[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(8): 1374-1379 (in Chinese). | |
41 | ZHOU Y, XIA Z X, LUO Z B, et al. Effect of three-electrode plasma synthetic jet actuator on shock wave control[J]. Science China Technological Sciences, 2017, 60(1): 146-152. |
42 | ZHOU Y, XIA Z X, LUO Z B, et al. Characterization of three-electrode SparkJet actuator for hypersonic flow control[J]. AIAA Journal, 2019, 57(2): 879-885. |
43 | HUANG H X, TAN H J, SUN S, et al. Letter: Transient interaction between plasma jet and supersonic compression ramp flow[J]. Physics of Fluids, 2018, 30(4): 041703. |
44 | WANG H Y, LI J, JIN D, et al. Effect of a transverse plasma jet on a shock wave induced by a ramp[J]. Chinese Journal of Aeronautics, 2017, 30(6): 1854-1865. |
45 | BOBASHEV S V, EROFEEV A V, LAPUSHKINA T A, et al. Effect of magnetohydrodynamics interaction in various parts of diffuser on inlet shocks: Experiment[J]. Journal of Propulsion and Power, 2005, 21(5): 831-837. |
46 | FOMICHEV V, YADRENKIN M, PODZIN V, et al. Flow settling over a wedge at the MHD-effect on a hypersonic air flow[C]∥ Proceedings of the 42nd AIAA Plasmadynamics and Lasers Conference. Reston: AIAA, 2011. |
47 | 李祝飞, 王军, 张志雨, 等. V形钝化前缘激波干扰问题[J]. 气动研究与实验, 2020, 32(1): 63-75. |
LI Z F, WANG J, ZHANG Z Y, et al. Shock interactions generated by V-shaped blunt leading edges[J]. Aerodynamic Research & Experiment, 2020, 32(1): 63-75 (in Chinese). | |
48 | 张英杰, 李祝飞, 张志雨, 等. 侧滑角对V字形钝化前缘激波振荡特性影响[J]. 推进技术, 2022, 43(11): 81-93. |
ZHANG Y J, LI Z F, ZHANG Z Y, et al. Effects of sideslip angle on shock oscillations of V-shaped blunt leading edge[J]. Journal of Propulsion Technology, 2022, 43(11): 81-93 (in Chinese). | |
49 | MARTINEZ-SCHRAMM J, EITELBERG G. Shock boundary layer interaction in hypersonic high enthalpy flow on a double wedge[C]∥ 22nd International Symposium on Shock Waves. London: Imperial College, 1999. |
50 | STARIKOVSKIY A, ALEKSANDROV N. Plasma-assisted ignition and combustion[J]. Progress in Energy and Combustion Science, 2013, 39(1): 61-110. |
51 | EGGERS T, DITTRICH R, VAVILL R. Numerical analysis of the SKYLON spaceplane in hypersonic flow: AIAA-2011-2298 [R]. Reston: AIAA, 2011. |
52 | 杨勇, 陈洪波. 高超声速再入飞行器IXV的研制与飞行试验[M]. 北京: 国防工业出版社, 2018. |
YANG Y, CHEN H B. Development and flight test of the intermediate experimental vehicle[M]. Beijing: National Defense Industry Press, 2018 (in Chinese). | |
53 | 姜宝森, 张亮, 李俊红, 等. 吸气式飞行器进气道唇口三维激波/激波干扰[J]. 航空动力学报, 2019, 34(4): 821-828. |
JIANG B S, ZHANG L, LI J H, et al. Three-dimensional shock/shock interaction of airbreathing vehicle’s inlet lip[J]. Journal of Aerospace Power, 2019, 34(4): 821-828 (in Chinese). | |
54 | GOONKO Y P, LATYPOV A F, MAZHUL I I, et al. Structure of flow over a hypersonic inlet with side compression wedges[J]. AIAA Journal, 2003, 41(3): 436-447. |
55 | ZHANG Z Y, LI Z F, YANG J M. Transitions of shock interactions on V-shaped blunt leading edges[J]. Journal of Fluid Mechanics, 2021, 912: A12. |
56 | WANG J, LI Z F, ZHANG Z Y, et al. Shock interactions on V-shaped blunt leading edges with various conic crotches[J]. AIAA Journal, 2020, 58(3): 1407-1411. |
57 | WANG J, LI Z F, YANG J M. Shock-induced pressure/heating loads on V-shaped leading edges with nonuniform bluntness[J]. AIAA Journal, 2021, 59(3): 1114-1118. |
58 | EDNEY B E. Effects of shock impingement on the heat transfer around blunt bodies[J]. AIAA Journal, 1968, 6(1): 15-21. |
59 | OLEJNICZAK J, WRIGHT M J, CANDLER G V. Numerical study of inviscid shock interactions on double-wedge geometries[J]. Journal of Fluid Mechanics, 1997, 352: 1-25. |
60 | WIETING A R. Multiple shock-shock interference on a cylindrical leading edge[J]. AIAA Journal, 1992, 30(8): 2073-2079. |
61 | PRABHU R, THAREJA R, WIETING A. Computational studies of a fluid spike as a leading edge protection device for shock-shock interference heating[C]∥ Proceedings of the 22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference. Reston: AIAA, 1991. |
62 | ALBERTSON C, VENKAT V. Shock interaction control for scramjet cowl leading edges[C]∥ AIAA/CIRA 13th International Space Planes and Hypersonics Systems and Technologies Conference. Reston: AIAA, 2005. |
63 | ADELGREN R G, YAN H, ELLIOTT G S, et al. Localized flow control by laser energy deposition applied to Edney IV shock impingement and intersecting shocks: 2003—0031[R]. Reston: AIAA, 2003. |
64 | ADELGREN R G, YAN H, ELLIOTT G S, et al. Control of Edney IV interaction by pulsed laser energy deposition[J]. AIAA Journal, 2005, 43(2): 256-269. |
65 | KNIGHT D, ADELGREN R G, ELLIOTT G S, et al. Laser energy deposition in Edney IV interaction[M]∥ Shock Waves. Berlin: Springer Berlin Heidelberg, 2005: 89-94. |
66 | YAN H, GAITONDE D. Control of Edney IV interaction by energy pulse: AIAA-2006-0562[R]. Reston: AIAA, 2006. |
67 | KOGAN M N, STARODUBTSEV M A. Reduction of peak heat fluxes by supplying heat to the free stream[J]. Fluid Dynamics, 2003, 38(1): 115-125. |
68 | 吴文堂, 洪延姬, 王殿恺, 等. 激光能量注入控制IV型激波干扰的数值研究[J]. 强激光与粒子束, 2014, 26(2): 50-55. |
WU W T, HONG Y J, WANG D K, et al. Numerical investigation of type IV shock interaction controlled by laser energy deposition[J]. High Power Laser and Particle Beams, 2014, 26(2): 50-55 (in Chinese). | |
69 | 王殿恺, 洪延姬, 任玉新, 等. 高重频激光控制IV型激波干扰方法研究[J]. 推进技术, 2015, 36(10): 1459-1464. |
WANG D K, HONG Y J, REN Y X, et al. Flow control method of type IV interaction with high rated laser energy[J]. Journal of Propulsion Technology, 2015, 36(10): 1459-1464 (in Chinese). | |
70 | XIE W, LUO Z B, ZHOU Y, et al. Experimental study on shock wave control in high-enthalpy hypersonic flow by using SparkJet actuator[J]. Acta Astronautica, 2021, 188: 416-425. |
71 | TANG M X, WU Y, WANG H Y. Experimental investigation on hypersonic shock-shock interaction control using plasma actuator array[J]. Acta Astronautica, 2022, 198: 577-586. |
72 | KONG Y K, LI J, WU Y, et al. Experimental study on shock-shock interaction over double wedge controlled by surface arc plasma array[J]. Contributions to Plasma Physics, 2022, 62(9): e202200062. |
73 | 张传标, 梁华, 郭善广, 等. 高能电弧等离子体激励控制双压缩拐角激波/边界层干扰实验研究[J]. 推进技术, 2022, 43(10): 213-228. |
ZHANG C B, LIANG H, GUO S G, et al. Experimental study on double compression ramp shock wave/boundary layer interaction controlled by high-energy streamwise pulsed arc discharge array[J]. Journal of Propulsion Technology, 2022, 43(10): 213-228 (in Chinese). | |
74 | 罗凯, 王永海, 汪球, 等. 高焓风洞中等离子体激励流动控制试验[J]. 航空学报, 2022, 43(S2): 92-99. |
LUO K, WANG Y H, WANG Q, et al. Plasma-actuated flow control test in high enthalpy shock tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(S2): 92-99 (in Chinese). | |
75 | SURZHIKOV S T. Hypersonic flow past sharp plate and double wedge with an electromagnetic actuator[J]. Fluid Dynamics, 2020, 55(6): 825-839. |
76 | 罗凯, 汪球, 李逸翔, 等. 基于高温气体效应的磁流体流动控制研究进展[J]. 力学学报, 2021, 53(6): 1515-1531. |
LUO K, WANG Q, LI Y X, et al. Research progress on magnetohydrodynamic flow control under test conditions with high temperature real gas effect[J]. Chinese Journal of Theoretical and Applied Mechanics, 2021, 53(6): 1515-1531 (in Chinese). | |
77 | 罗凯, 汪球, 李进平, 等. 基于高温真实气体效应的双锥磁流体流动控制[J]. 航空学报, 2022, 43(S2): 79-91. |
LUO K, WANG Q, LI J P, et al. Magnetohydrodynamic flow control of double-cone under high temperature real gas effect[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(S2): 79-91 (in Chinese). | |
78 | LI S, YAN C, KANG D K, et al. Investigation of flow control methods for reducing heat flux on a V-shaped blunt leading edge under real gas effects[J]. Physics of Fluids, 2023, 35(3): 036113. |
79 | 范孝华, 唐志共, 王刚, 等. 激波/湍流边界层干扰低频非定常性研究评述[J]. 航空学报, 2022, 43(1): 625917. |
FAN X H, TANG Z G, WANG G, et al. Review of low-frequency unsteadiness in shock wave/turbulent boundary layer interaction[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(1): 625917 (in Chinese). | |
80 | 时晓天, 吕蒙, 赵渊, 等. 激波/湍流边界层干扰的流动控制技术综述[J]. 航空学报, 2022, 43(1): 625929. |
SHI X T, LYU M, ZHAO Y, et al. Flow control technique for shock wave/turbulent boundary layer interactions[J]. Acta Aeronautica et Astronautica Sinica, 2022, 43(1): 625929 (in Chinese). | |
81 | 吴瀚, 王建宏, 黄伟, 等. 激波/边界层干扰及微型涡流发生器控制研究进展[J]. 航空学报, 2021, 42(6): 025371. |
WU H, WANG J H, HUANG W, et al. Research progress on shock wave/boundary layer interactions and flow controls induced by micro vortex generators[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(6): 025371 (in Chinese). | |
82 | 张悦, 谭慧俊, 王子运, 等. 进气道内激波/边界层干扰及控制研究进展[J]. 推进技术, 2020, 41(2): 241-259. |
ZHANG Y, TAN H J, WANG Z Y, et al. Progress of shock wave/boundary layer interaction and its control in inlet[J]. Journal of Propulsion Technology, 2020, 41(2): 241-259 (in Chinese). | |
83 | VERMA S B, MANISANKAR C. Shock wave/boundary-layer interaction control on a compression ramp using steady micro jets[J]. AIAA Journal, 2012, 50(12): 2753-2764. |
84 | DU Z B, SHEN C B, HUANG W, et al. Control mechanism of the three-dimensional shock wave/boundary layer interaction with the steady and pulsed micro-jets in a supersonic crossflow[J]. Physics of Fluids, 2022, 34(8): 086109. |
85 | 徐浩, 杜兆波, 钟翔宇, 等. 超声速气流中激波/边界层干扰微射流控制研究进展[J]. 航空兵器, 2022, 29(4): 83-90. |
XU H, DU Z B, ZHONG X Y, et al. Research progress of microjet control of shock wave/boundary layer interactions in supersonic flow field[J]. Aero Weaponry, 2022, 29(4): 83-90 (in Chinese). | |
86 | LIU Q, LUO Z B, DENG X, et al. Fine structures of self-sustaining dual jets in supersonic crossflow[J]. Acta Astronautica, 2019, 164: 262-267. |
87 | LIU Q, LUO Z B, DENG X, et al. Vortical structures and density fluctuations analysis of supersonic forward-facing step controlled by self-sustaining dual synthetic jets[J]. Acta Mechanica Sinica, 2020, 36(6): 1215-1227. |
88 | LIU Q, XIE W, LUO Z B, et al. Flow structures and unsteadiness in hypersonic shock wave/turbulent boundary layer interaction subject to steady jet[J]. Acta Mechanica Sinica, 2023, 39(5): 323202. |
89 | DU Z B, SHEN C B, SHEN Y, et al. Design exploration on the shock wave/turbulence boundary layer control induced by the secondary recirculation jet[J]. Acta Astronautica, 2021, 181: 468-481. |
90 | 严红, 王松. 热激励在超声速进气道内对激波诱导的边界层分离的控制机理[J]. 空气动力学学报, 2014, 32(6): 806-813. |
YAN H, WANG S. Control of shock/boundary layer interaction in supersonic inlet using thermal excitation[J]. Acta Aerodynamica Sinica, 2014, 32(6): 806-813 (in Chinese). | |
91 | TANG M X, WU Y, GUO S G, et al. Compression ramp shock wave/boundary layer interaction control with high-frequency streamwise pulsed spark discharge array[J]. Physics of Fluids, 2020, 32(12): 121704. |
92 | MA X G, FAN J A, WU Y K, et al. Flow control effect of pulsed arc discharge plasma actuation on impinging shock wave/boundary layer interaction[J]. Physics of Fluids, 2023, 35(3): 036110. |
93 | GAN T, WANG Q. Mechanisms of SWBLI control by using a surface arc plasma actuator array[J]. Experimental Thermal and Fluid Science, 2021, 128: 110428. |
94 | ZHANG C B, YANG H S, LIANG H, et al. Plasma-based experimental investigation of double compression ramp shock wave/boundary layer interaction control[J]. Journal of Physics D: Applied Physics, 2022, 55(32): 325202. |
95 | 王林, 罗振兵, 夏智勋, 等. 高速流场主动流动控制激励器研究进展[J]. 中国科学: 技术科学, 2012, 42(10): 1103-1119. |
WANG L, LUO Z B, XIA Z X, et al. Research progress of active flow control actuator for high-speed flow field[J]. Scientia Sinica (Technologica), 2012, 42(10): 1103-1119 (in Chinese). | |
96 | NARAYANASWAMY V, RAJA L L, CLEMENS N T. Control of unsteadiness of a shock wave/turbulent boundary layer interaction by using a pulsed-plasma-jet actuator[J]. Physics of Fluids, 2012, 24(7): 076101. |
97 | WANG H Y, LI J, JIN D, et al. High-frequency counter-flow plasma synthetic jet actuator and its application in suppression of supersonic flow separation[J]. Acta Astronautica, 2018, 142: 45-56. |
98 | LUO Y H, LI J, LIANG H, et al. Suppressing unsteady motion of shock wave by high-frequency plasma synthetic jet[J]. Chinese Journal of Aeronautics, 2021, 34(9): 60-71. |
99 | 马正雪. 火花放电合成射流及其激波/边界层干扰控制直接数值模拟研究[D]. 长沙: 国防科技大学, 2022. |
MA Z X. Direct numerical simulation study of SparkJet and its shock wave/boundary layer interference control[D]. Changsha: National University of Defense Technology, 2022 (in Chinese). | |
100 | MEARS L, ARORA N, ALⅥ F S. Introducing controlled perturbations in a 3-D swept shock boundary layer interaction[C]∥ Proceedings of the 2018 AIAA Aerospace Sciences Meeting. Reston: AIAA, 2018. |
101 | DESHPANDE A S, POGGIE J. Flow control of swept shock-wave/boundary-layer interaction using plasma actuators[J]. Journal of Spacecraft and Rockets, 2018, 55(5): 1198-1207. |
102 | YANG H S, ZONG H H, LIANG H, et al. Swept shock wave/boundary layer interaction control based on surface arc plasma[J]. Physics of Fluids, 2022, 34(8): 087119. |
103 | 张刘, 黄勇, 陈辅政, 等. 基于环量控制的无尾飞翼俯仰和滚转两轴无舵面姿态控制飞行试验[J]. 航空学报, 2023, 44(22): 128224. |
ZHANG L, HUANG Y, CHEN F Z, et al. Rudderless at titude control flight test based on circulation control of tail-less flying wing in pitch and roll axes[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(22): 128224 (in Chinese). | |
104 | LUO Z B, ZHAO Z J, LIU J F, et al. Novel roll effector based on zero-mass-flux dual synthetic jets and its flight test[J]. Chinese Journal of Aeronautics, 2022, 35(8): 1-6. |
105 | 赵志杰, 罗振兵, 刘杰夫, 等. 基于分布式合成双射流的飞行器无舵面三轴姿态控制飞行试验[J]. 力学学报, 2022, 54(5): 1220-1228. |
ZHAO Z J, LUO Z B, LIU J F, et al. Flight test of aircraft three-axis attitude control without rudders based on distributed dual synthetic jets[J]. Chinese Journal of Theoretical and Applied Mechanics, 2022, 54(5): 1220-1228 (in Chinese). | |
106 | Air & Space Forces Association[EB/OL]. [2023-05-16]. . |
107 | 张伟伟, 寇家庆, 刘溢浪. 智能赋能流体力学展望[J]. 航空学报, 2021, 42(4): 524689. |
ZHANG W W, KOU J Q, LIU Y L. Prospect of artificial intelligence empowered fluid mechanics[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(4): 524689 (in Chinese). | |
108 | 任峰, 高传强, 唐辉. 机器学习在流动控制领域的应用及发展趋势[J]. 航空学报, 2021, 42(4): 524686. |
REN F, GAO C Q, TANG H. Machine learning for flow control: Applications and development trends[J]. Acta Aeronautica et Astronautica Sinica, 2021, 42(4): 524686 (in Chinese). | |
109 | FERNEX D, NOACK B R, SEMAAN R. Cluster-based network modeling—From snapshots to complex dynamical systems[J]. Science Advances, 2021, 7(25): eabf5006. |
110 | CORNEJO MACEDA G Y, VARON E, LUSSEYRAN F, et al. Stabilization of a multi-frequency open cavity flow with gradient-enriched machine learning control[J]. Journal of Fluid Mechanics, 2023, 955: A20. |
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