[1] |
WARSOP C, CROWTHER W J. Fluidic flow control effectors for flight control[J]. AIAA Journal, 2018, 56(10): 3808–3824. doi: 10.2514/1.J056787
|
[2] |
FIELDING J, LAWSON C, MARTINS-PIRES R, et al. Design, build and flight of the DEMON demonstrator UAV[C]//Proc of the 11th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference. 2011: 6963. doi: 10.2514/6.2011-6963.
|
[3] |
WARSOP C, CROWTHER W. NATO AVT-239 Task Group: Flight demonstration of fluidic flight controls on the MAGMA subscale demonstrator Aircraft[C]//Proc of the AIAA Scitech 2019 Forum. 2019: 0282. doi: 10.2514/6.2019-0282.
|
[4] |
HENRI C. Device for deflecting a stream of elastic fluid projected into an elastic fluid: US2052869[P]. 1936-09-01.
|
[5] |
REBA I. Applications of the coanda effect[J]. Scientific American, 1966, 214(6): 84–92. doi: 10.1038/scientificamerican0666-84
|
[6] |
ENGLAR R J. Experimental investigation of the high velocity Coanda wall jet applied to bluff trailing edge circulation control airfoils[R]. NASA STI/Recon Technical Report N, 1975, 76: 26438.
|
[7] |
ABRAMSON J, ROGERS E. High-speed characteristics of circulation control airfoils[C]//Proc of the 21st Aerospace Sciences Meeting. 1983: 265. doi: 10.2514/6.1983-265
|
[8] |
WOOD N, NIELSEN J. Circulation control airfoils - Past, present, future[C]//Proc of the 23rd Aerospace Sciences Meeting. 1985: 204. doi: 10.2514/6.1985-204.
|
[9] |
ENGLAR R. Circulation control pneumatic aerodynamics: blown force and moment augmentation and modification - Past, present and future[C]//Proc of the Fluids 2000 Conference and Exhibit. 2000: 2541. doi: 10.2514/6.2000-2541.
|
[10] |
JONES G, VIKEN S, WASHBURN A, et al. An active flow circulation controlled flap concept for general aviation aircraft applications[C]//Proc of the 1st Flow Control Conference. 2002: 3157. doi: 10.2514/6.2002-3157.
|
[11] |
SHI Z W, ZHU J C, DAI X X, et al. Aerodynamic characteristics and flight testing of a UAV without control surfaces based on circulation control[J]. Journal of Aerospace Engineering, 2019, 32(1): 4018134.1–4018134.23. doi: 10.1061/(asce)as.1943-5525.0000947
|
[12] |
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. doi: 10.1016/j.cja.2021.08.015
|
[13] |
雷玉昌, 张登成, 张艳华, 等. 超临界翼型的双射流环量控制研究[J]. 飞行力学, 2020, 38(4): 16–21. doi: 10.13645/j.cnki.f.d.20200602.010LEI Y C, ZHANG D C, ZHANG Y H, et al. Circulation control of double jet flow on supercritical airfoil[J]. Flight Dynamics, 2020, 38(4): 16–21. doi: 10.13645/j.cnki.f.d.20200602.010
|
[14] |
王磊, 杜海, 李秋实, 等. 环量控制机翼增升及滚转控制特性研究[J]. 空气动力学学报, 2021, 39(1): 43–51. doi: 10.7638/kqdlxxb-2019.0069WANG L, DU H, LI Q S, et al. Research on the lift-enhancement and roll control characteristics of a circulation control wing[J]. Acta Aerodynamica Sinica, 2021, 39(1): 43–51. doi: 10.7638/kqdlxxb-2019.0069
|
[15] |
雷玉昌, 张登成, 张艳华. 环量控制翼型非定常气动力建模[J]. 北京航空航天大学学报, 2021, 47(10): 2138–2148. doi: 10.13700/j.bh.1001-5965.2020.0360LEI Y C, ZHANG D C, ZHANG Y H. Unsteady aerodynamic modeling of circulation control airfoil[J]. Journal of Beijing University of Aeronautics and Astronautics, 2021, 47(10): 2138–2148. doi: 10.13700/j.bh.1001-5965.2020.0360
|
[16] |
雷玉昌, 张登成, 张艳华, 等. 脉冲射流对环量控制翼型气动性能的影响[J]. 北京航空航天大学学报, 2022, 48(3): 485–494. doi: 10.13700/j.bh.1001-5965.2020.0560LEI Y C, ZHANG D C, ZHANG Y H, et al. Effect of pulsed jet on aerodynamic performance of circulation control airfoil[J]. Journal of Beijing University of Aeronautics and Astronautics, 2022, 48(3): 485–494. doi: 10.13700/j.bh.1001-5965.2020.0560
|
[17] |
BARHAM R. Thrust vector aided maneuvering of the YF-22 Advanced Tactical Fighter prototype[C]//Proc of the Biennial Flight Test Conference. 1994: 2105. doi: 10.2514/6.1994-2105.
|
[18] |
肖中云, 江雄, 牟斌, 等. 流体推力矢量技术研究综述[J]. 实验流体力学, 2017, 31(4): 8–15. doi: 10.11729/syltlx20160207XIAO Z Y, JIANG X, MOU B, et al. Advances influidic thrust vectoring technique research[J]. Journal of Experi-ments in Fluid Mechanics, 2017, 31(4): 8–15. doi: 10.11729/syltlx20160207
|
[19] |
DEERE K. Summary of fluidic thrust vectoring research at NASA langley research center[C]//Proc of the 21st AIAA Applied Aerodynamics Conference. 2003: 3800. doi: 10.2514/6.2003-3800.
|
[20] |
FLAMM J D, DEERE K A, BERRIER B L, et al. Experimental study of a dual-throat fluidic thrust-vectoring nozzle concept[C]//Proc of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2005: 3503. doi: 10.2514/6.2005-3503.
|
[21] |
DENG R Y, SETOGUCHI T, DONG KIM H. Large eddy simulation of shock vector control using bypass flow passage[J]. International Journal of Heat and Fluid Flow, 2016, 62: 474–481. doi: 10.1016/j.ijheatfluidflow.2016.08.011
|
[22] |
MILLER D, YAGLE P, HAMSTRA J. Fluidic throat skewing for thrust vectoring in fixed-geometry nozzles[C]// Proc of the 37th Aerospace Sciences Meeting and Exhibit. 1999: 365. doi: 10.2514/6.1999-365.
|
[23] |
WASHINGTON D M, ALVI F S, STRYKOWSKI P J, et al. Multiaxis fluidic thrust vector control of a supersonic jet using counterflow[J]. AIAA Journal, 1996, 34(8): 1734–1736. doi: 10.2514/3.13296
|
[24] |
DEERE K A, BERRIER B L, FLAMM J D, et al. A computational study of a dual throat fluidic thrust vectoring nozzle concept[C]//Proc of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2005: 3502. doi: 10.2514/6.2005-3502.
|
[25] |
SUNG H G, HEO J Y. Fluidic thrust vector control of supersonic jet using coflow injection[J]. Journal of Propul-sion and Power, 2012, 28(4): 858–861. doi: 10.2514/1.B34266
|
[26] |
MASON M, CROWTHER W. Fluidic thrust vectoring for low observable air vehicles[C]//Proc of the 2nd AIAA Flow Control Conference. 2004: 2210. doi: 10.2514/6.2004-2210
|
[27] |
SONG M, PARK S, LEE Y. Application of backstep coanda flap for supersonic coflowing fluidic thrust-vector control[J]. AIAA Journal, 2014, 52(10): 2355–2359. doi: 10.2514/1.J052971
|
[28] |
龚东升. 基于微型涡喷发动机的无源流体推力矢量喷管的研究[D]. 南京: 南京航空航天大学硕士学位论文, 2020.GONG D S. Research on passive fluid thrust vector nozzle based on micro turbojet engine[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2020.
|
[29] |
龚东升, 顾蕴松, 周宇航, 等. 基于微型涡喷发动机热喷流的无源流体推力矢量喷管的控制规律[J]. 航空学报, 2020, 41(10): 101–112. doi: 10.7527/S1000-6893.2019.23609GONG D S, GU Y S, ZHOU Y H, et al. Control law of passive fluid thrust vector nozzle based on thermal jet of micro turbojet engine[J]. Acta Aeronautica et Astronautica Sinica, 2020, 41(10): 101–112. doi: 10.7527/S1000-6893.2019.23609
|
[30] |
冯潮, 顾蕴松, 方瑞山, 等. 水下无源流体推力矢量喷管流动特性研究[J]. 实验流体力学.FENG C, GU Y S, FANG R S, et al. Research on flow characteristics of underwater passive fluidic thrust vectoring nozzle[J]. Journal of Experiments in Fluid Mechanics. doi: 10.11729/syltlx20220071
|
[31] |
肖中云, 顾蕴松, 江雄, 等. 一种基于引射效应的流体推力矢量新技术[J]. 航空学报, 2012, 33(11): 1967–1974. doi: 10.3321/j.issn:1000-6893.2008.04.001XIAO Z Y, GU Y S, JIANG X, et al. A new fluidic thrust vectoring technique based on ejecting mixing effects[J]. Acta Aeronautica et Astronautica Sinica, 2012, 33(11): 1967–1974. doi: 10.3321/j.issn:1000-6893.2008.04.001
|
[32] |
耿令波, 胡志强, 林扬, 等. 基于横向二次射流的水下推力矢量方法[J]. 航空动力学报, 2017, 32(8): 1922–1932. doi: 10.13224/j.cnki.jasp.2017.08.016GENG L B, HU Z Q, LIN Y, et al. Underwater thrust vectoring method based on cross second flow[J]. Journal of Aerospace Power, 2017, 32(8): 1922–1932. doi: 10.13224/j.cnki.jasp.2017.08.016
|
[33] |
YAROS S F, SEXSTONE M G, HUEBNER L D, et al. Synergistic Airframe-Propulsion Interactions and Integra-tions: A White Paper Prepared by the 1996-1997 Langley Aeronautics Technical Committee[R]. NASA/TM-1998-207644, 1998.
|
[34] |
JONES G S, ENGLAR R J. Advances in pneumatic controlled high lift systems through pulsed blowing[C]//Proc of the 21st AIAA Applied Aerodynamics Conference. 2003: 3411. doi: 10.2514/6.2003-3411.
|
[35] |
JONES A, EDSTRAND A, CHANDRAN M, et al. An experimental investigation of unsteady and steady circulation control for an elliptical airfoil[C]//Proc of the 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition. 2010. doi: 10.2514/6.2010-346.
|
[36] |
PACK L G, SEIFERT A. Periodic excitation for jet vectoring and enhanced spreading[J]. Journal of Aircraft, 2001, 38(3): 486–495. doi: 10.2514/2.2788
|
[37] |
WOSZIDLO R, OSTERMANN F, SCHMIDT H J. Fundamental properties of fluidic oscillators for flow control applications[J]. AIAA Journal, 2019, 57(3): 978–992. doi: 10.2514/1.J056775
|
[38] |
BOBUSCH B C, WOSZIDLO R, BERGADA J M, et al. Experimental study of the internal flow structures inside a fluidic oscillator[J]. Experiments in Fluids, 2013, 54(6): 1559. doi: 10.1007/s00348-013-1559-6
|
[39] |
GAERTLEIN S, WOSZIDLO R, OSTERMANN F, et al. The time-resolved internal and external flow field properties of a fluidic oscillator[C]//Proc of the 52nd Aerospace Sciences Meeting. 2014: 1143. doi: 10.2514/6.2014-1143.
|
[40] |
OSTERMANN F, WOSZIDLO R, NAYERI C, et al. Experimental comparison between the flow Field of two common fluidic oscillator designs[C]//Proc of the 53rd AIAA Aerospace Sciences Meeting. 2015: 0781. doi: 10.2514/6.2015-0781.
|
[41] |
LI Z Y, LIU J J, ZHOU W W, et al. Experimental investigation of flow dynamics of sweeping jets impinging upon confined concave surfaces[J]. International Journal of Heat and Mass Transfer, 2019, 142: 118457. doi: 10.1016/j.ijheatmasstransfer.2019.118457
|
[42] |
GREGORY J W, SULLIVAN J P, RAMAN G, et al. Characterization of the microfluidic oscillator[J]. AIAA Journal, 2007, 45(3): 568–576. doi: 10.2514/1.26127
|
[43] |
MELTON L P, KOKLU M, ANDINO M, et al. Active flow control via discrete sweeping and steady jets on a simple-hinged flap[J]. AIAA Journal, 2018, 56(8): 2961–2973. doi: 10.2514/1.j056841
|
[44] |
RAMAN G, RAGHU S. Miniature fluidic oscillators for flow and noise control - Transitioning from macro to micro fluidics[C]//Proc of the Fluids 2000 Conference and Exhibit. 2000: 2554. doi: 10.2514/6.2000-2554.
|
[45] |
SCHMIDT H -J, WOSZIDLO R, NAYERI C N, et al. Drag reduction on a rectangular bluff body with base flaps and fluidic oscillators[J]. Experiments in Fluids, 2015, 56(7): 151. doi: 10.1007/s00348-015-2018-3
|
[46] |
GUYOT D, BOBUSCH B, PASCHEREIT C O, et al. Active combustion control using a fluidic oscillator for asymmetric fuel flow modulation[C]//Proc of the 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2008: 4956. doi: 10.2514/6.2008-4956.
|
[47] |
ZHOU W, YUAN L, LIU Y, et al. Heat transfer of a sweeping jet impinging at narrow spacings[J]. Experimental Thermal and Fluid Science, 2019, 103: 89–98. doi: 10.1016/j.expthermflusci.2019.01.007
|
[48] |
DENNAI B, BENTALEB A, CHEKIFI T, et al. Micro fluidic oscillator: a technical solution for micro mixture[J]. Advanced Materials Research, 2014, 1064: 213–218. doi: 10.4028/www.scientific.net/amr.1064.213
|
[49] |
周銮良, 王士奇, 温新. 高频高速流体振荡器工作特性[J]. 航空动力学报, 2022, 37(4): 877–885. doi: 10.13224/j.cnki.jasp.20210099ZHOU L L, WANG S Q, WEN X. Working characteristics of a fluidic oscillator with high frequency and high speed[J]. Journal of Aerospace Power, 2022, 37(4): 877–885. doi: 10.13224/j.cnki.jasp.20210099
|
[50] |
ZHOU L L, WANG S Q, SONG J S, et al. Study of internal time-resolved flow dynamics of a subsonic fluidic oscillator using fast pressure sensitive paint[J]. Experiments in Fluids, 2022, 63(1): 17. doi: 10.1007/s00348-021-03370-w
|
[51] |
OSTERMANN F, WOSZIDLO R, NAYERI C N, et al. Properties of a sweeping jet emitted from a fluidic oscillator[J]. Journal of Fluid Mechanics, 2018, 857: 216–238. doi: 10.1017/jfm.2018.739
|
[52] |
ADHIKARI A, SCHWEITZER T, LÜCKOFF F, et al. Design of a fluidic actuator with independent frequency and amplitude modulation for control of swirl flame dynamics[J]. Fluids, 2021, 6(3): 128. doi: 10.3390/fluids6030128
|
[53] |
CAPOBIANCO V, SHANKAR P, JIANG M. Effect of slot height variation on the aerodynamic performance of a circulation control airfoil: a CFD analysis[C]//Proc of the AIAA Scitech 2019 Forum. 2019: 0579. doi: 10.2514/6.2019-0579.
|
[54] |
JONES G S, MILHOLEN W E, CHAN D T, et al. A sweeping jet application on a high Reynolds number semi-span supercritical wing configuration[C]//Proc of the 35th AIAA Applied Aerodynamics Conference. 2017: 3044. doi: 10.2514/6.2017-3044.
|
[55] |
JENTZSCH M, TAUBERT L, WYGNANSKI I. Using sweeping jets to trim and control a tailless aircraft model[J]. AIAA Journal, 2019, 57(6): 2322–2334. doi: 10.2514/1.j056962
|
[56] |
LI Z Y, LIU Y D, ZHOU W W, et al. Lift augmentation potential of the circulation control wing driven by sweeping jets[J]. AIAA Journal, 2022, 60(8): 4677–4698. doi: 10.2514/1.J061456
|
[57] |
TEN J S, POVEY T. Self-Excited Fluidic Oscillators for gas turbines cooling enhancement: experimental and computa-tional study[J]. Journal of Thermophysics and Heat Transfer, 2018, 33(2): 536–547. doi: 10.2514/1.T5261
|
[58] |
BORGMANN D, PANDE A, LITTLE J C, et al. Experimental study of discrete jet forcing for flow separation control on a wall mounted hump[C]//Proc of the 55th AIAA Aerospace Sciences Meeting. 2017: 1450. doi: 10.2514/6.2017-1450.
|
[59] |
WEN X, ZHOU K W, LIU P C, et al. Schlieren visualization of coflow fluidic thrust vectoring using sweeping jets[J]. AIAA Journal, 2021: 1-10. doi: 10.2514/1.J060805.
|
[60] |
DORES D, MADRUGA SANTOS M M, KROTHAPALLI A, et al. Characterization of a counterflow thrust vectoring scheme on a gas turbine engine exhaust jet[C]//Proc of the 3rd AIAA Flow Control Conference. 2006: 3516. doi: 10.2514/6.2006-3516.
|