Study of Low Speed Wind Tunnel Test Using Microsecond Pulsed Plasma Actuation on Flying Wing Model
1.Low Speed and High Reynolds Aeronautics Laboratory,AVIC Aerodynamics Research Institute,Harbin 5000,China;2.Aeronautics and Astronautics Engineering College,Air Force Engineering University,Xi’an 710038,China
NIU Zhong-guo1,2,HU Qiu-qi1,LIANG Hua2,LIU Jie1,XU Xiang-hui1,JIANG Jia-li1. Study of Low Speed Wind Tunnel Test Using Microsecond Pulsed Plasma Actuation on Flying Wing Model[J]. Journal of Propulsion Technology, 2019, 40(12): 2821-2831.
[1] 许晓平, 周 洲 . 飞翼布局无人机流动分离控制及机理分析[J]. 力学学报, 2014, 46(4):497-504.
[2] 王豪杰, 李 杰, 周 洲 . 飞翼类特殊布局无人机气动力设计研究[J]. 西北工业大学学报, 2011, 29(5):789-793.
[3] 程雪梅 . 飞翼布局无人机的稳定与操纵特性分析研究[J]. 飞行力学, 2011, 29(1): 9-12.
[4] 屈晓波, 章卫国, 蔡涪育, 等 . 基于特征结构配置的飞翼无人机纵向控制律设计与试飞验证[J]. 计算机测量与控制, 2015, 23(2): 494-496.
[5] 牛中国, 许相辉, 蒋甲利, 等 . 飞翼模型等离子体控制PIV试验研究[C]. 太原:非接触流动显示与测量技术专题学术研讨会, 2017.
[6] Nangia Dr R K , Palmer Dr M E . Flying Wings (Blended Wing Bodies) with AFT- & Forward- Sweep Relating Design Camber & Twist to Longitudinal Control[C]. California: AIAA Atmospheric Flight Mechanics Conference & Exhibit, 2002.
[7] Patel M P , Ng T T , Vasudevan S . Plasma Actuators for Hingeless Aerodynamic Control of an Unmanned Air Vehicle[J]. Journal of Aircraft, 2007, 44(4): 1264-1274.
[8] 战培国, 程娅红, 赵 昕 . 主动流动控制技术研究[J]. 航空科学技术, 2010, (5): 2-6.
[9] Wu Y , Li Y H . Progress and Outlook of Plasma Flow Control[J]. Acta Aeronautica Et Astronautica Sinica, 2015, 36(2): 381-405.
[10] Zhao Zi-jie , Li Jiun-Ming , Zheng Jian-guo , et al . Study of Shock and Induced Flow Dynamics by Nanosecond Dielectric-Barrier-Discharge Plasma Actuators[J].AIAA Journal, 2014, 53(5):1336-1348.
[11] 张 鑫, 黄 勇, 王勋年, 等 . 超临界机翼介质阻挡放电等离子体流动控制[J]. 航空学报, 2016, 37(6):1733-1742.
[12] 史志伟, 杜 海, 李 铮, 等 . 等离子体流动控制技术原理及典型应用[J]. 高压电器, 2017, 53(4):0072-0078.
[13] 李应红, 吴 云, 梁 华, 等 . 提高抑制流动分离能力的等离子体冲击流动控制原理[J]. 科学通报, 2010, 55(31): 3060-3068.
[14] 杜 海, 史志伟, 程克明, 等 . 纳秒脉冲等离子体分离流控制频率优化及涡运动过程分析[J]. 航空学报, 2016, 37(7): 2102-2111.
[15] 郝琳召, 张彬乾, 陈真利 . 纳秒等离子体激励控制翼型流动分离机理研究[J]. 航空工程进展, 2014, 5(1): 25-32.
[16] Shang J S . Validation of Plasma Injection for Hypersonic Blunt-Body Drag Reduction[C]. Paris: RTO AVT, 2012.
[17] Kozlov A V , Thomas F O . Active Noise Control of Bluff-Body Flows Using Dielectric Barrier Discharge Plasma Actuators[C]. Miami: 30th AIAA Aeroacoustics Conference, 2009.
[18] Christopher Ali Merchant . Active Noise Control Using Glow Discharge Plasma Panels[D]. Cambridge: Master of Science at the Massachusetts Institute of Technology, 2001.
[19] Dennis K , Suzen Y B . Simulations of Plasma Flow Control in Low-Pressure Turbines[R]. AIAA 2008-543.
[20] Daniel VN , Thomas C . Tip Clearance Flow Control in a Linear Turbine Cascade Using Plasma Actuation[R]. AIAA 2009-300.
[21] Daniel K , Corke Thomas C , Scott C . Turbine Tip Clearance Flow Control Using Plasma Actuators[R]. AIAA 2006-21.
[22] Little J , Takashima K , Nishihara M , et al . Separation Control with Nanosecond-Pulse-Driven Dielectric Barrier Discharge Plasma Actuators[J]. AIAA Journal, 2012, 50(2): 350-365.
[23] Grundmann Sven , Tropea Cameron . Delay of Boundary-Layer Transition Using Plasma Actuators[R]. AIAA2008-1369.
[24] Roth J R , Sherman D M , Wilkinson Stephen P , et al . Boundary Layer Flow Control with a One Atmosphere Uniform Glow Discharge Surface Plasma[R]. AIAA98-0328.
[25] Roth J R , Knoxville . Aerodynamic Flow Acceleration Using Paraelectric and Peristaltic Electrohydrodynamic Effects of a One Atmosphere Uniform Glow Discharge Plasma[J]. Physics of Plasmas, 2003, 10(5): 2117-2126.
[26] 潘 波, 沈锦明, 林 麒 . 等离子体激励器流场测量及诱导推力实验[J]. 推进技术, 2011, 32(1): 146-150. (PAN Bo, SHEN Jin-ming, LIN Qi. Experiment on Flow Field and Thrust Induced by Plasma Actuators[J]. Jounal of Propulsion Technology, 2011, 32(1):146-150.)
[27] Seifert A , Pack L G . Oscillatory Excitation of Unsteady Compressible Flows over Airfoils at Flight Reynolds Numbers[R]. AIAA99-0925.
[28] Roupassov D V , Nikipelov A A , Nudnova M M , et al . Flow Separation Control by Plasma Actuator with Nanosecond Pulse-Periodic Discharge[J]. AIAA Journal, 2009, 47(1): 168-185.
[29] Zhao G , Li Y , Hua L , et al . Flow Separation Control on Swept Wing with Nanosecond Pulse Driven DBD Plasma Actuators[J]. Chinese Journal of Aeronautics, 2015, 28(2): 368-376.
[30] Post M L , Corke T C . Separation Control on High Angle of Attack Airfoil Using Plasma Actuators[J]. AIAA Journal, 2012, 42(11): 2177-2184
[31] Rethmel C . Airfoil Leading Edge Flow Separation Control Using Nanosecond Pulse DBD Plasma Actuators[D]. Columbus: The Ohio State University, 2011.
[32] 梁 华, 李应红 . 等离子体气动激励抑制翼型失速分离的仿真研究[J]. 航空动力学报, 2008, 23(5): 777-783.
[33] 李应红, 梁 华, 马清源, 等 . 脉冲等离子体气动激励抑制翼型吸力面流动分离的实验[J]. 航空学报, 2008, 29(6): 1429-1435.
[34] Patel M , Sowle Z , Corke T C , et al . Autonomous Sensing and Control of Wing Stall Using a Smart Plasma Slat[J]. Journal of Aircraft, 2007, 44(2): 516-527.
[35] 张 鑫, 黄 勇, 沈志洪, 等 . 高风速下介质阻挡放电等离子体气动激励抑制翼-身组合体失速分离的试验研究[J]. 实验流体力学, 2012, 26(3): 17-20.
[36] 牛中国, 于金革, 孙 楠, 等 . 飞机模型等离子体力流动控制技术研究[C]. 西安: 中国力学大会, 2013.
[37] 牛中国, 孙 楠, 孙 健, 等 . 三角翼模型等离子体流动控制技术研究[C]. 上海:中国力学大会, 2015.
[38] 刘汝兵, 孙 伟, 牛中国, 等 . 火花放电等离子体射流实验研究[J]. 推进技术, 2015, 36(3): 372-377.
[39] Lopera J , Ng T T , Corke T C . Aerodynamic Control of 1303 UAV Using Windward Surface Plasma Actuators on a Separation Ramp[J]. Journal of Aircraft, 2007, 44(6): 1889-1895.
[40] 牛中国, 孙 建, 孙 楠, 等 . 大展弦比飞翼模型失速特性等离子体控制风洞试验研究[C]. 成都:第十七届全国等离子体科学技术会议, 2015.
[41] 姚军锴, 何海波, 周丹杰, 等 . 飞翼布局飞行器等离子体激励滚转操控试验[J]. 北京航空航天大学学报, 2017, 43(4):701-708.
[42] 马 杰, 梁 华, 吴 云, 等 . 毫秒脉冲等离子体激励改善飞翼的气动性能实验[J]. 航空动力学报, 2016, 31(8): 1845-1851.
[43] 范洁川 . 风洞试验手册[M]. 北京:航空工业出版社, 2012.
[44] 李周复 . 风洞试验手册[M]. 北京:航空工业出版社, 2015.