鸭式布局飞机矢量喷流对地面效应影响的风洞试验

doi:10.7527/S1000-6893.2019.23031

Abstract

Abstract: An experimental study of single-engine canard aircraft interactive behaviors between vectoring jet and ground effect is conducted in the low-speed wind tunnel. The results indicate that jets can enhance the ground effect of the aircraft, increase the lift coefficient, reduce flight velocity of take-off/landing, and shorten the distance of take-off/landing, improving the performance of take-off/landing. When the nozzle of vectoring engine is deflected upward or downward, the airflows induced by vectoring jets in the upper and lower surface of the aircraft are asymmetrical, reducing the increments of drag coefficient caused by ground effect. On this basis, the flow field mechanism of interactive behaviors between vectoring jet and ground effect is analyzed by numerical simulation.

Key words: canard configuration, thrust vectoring, wind tunnel test, ground effect, jet

CLC Number:

V211.4

WEI Zhongcheng, WANG Jinjun, YUAN Bing. Wind tunnel test of canard aircraft interactive behaviors between vectoring jet and ground effect[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2019, 40(11): 123031-123031.

References 21

[1]	GILYARD G B, BOLONKIN A. Optimal pitch thrust-vector angle and benefits for all flight regimes:NASA/TM-2000-209021[R]. Washington, D.C.:NASA, 2003.
[2]	赵群力. 推力矢量在战斗机上的应用[J]. 国际航空, 1999(1):20-23. ZHAO Q L. The application of thrust vectoring on fighters[J]. International Aviation, 1999(1):20-23(in Chinese).
[3]	BURSEY R, DICKINSON R. Flight test result of the F-15S/MTD thrust vectoring/thrust reversing exhaust nozzle:AIAA-1990-1906[R]. Reston, VA:AIAA, 1990.
[4]	方昌德. 飞机推力矢量技术发展综述[J]. 航空科学技术,1998(2):10-12. FANG C D. Developing status of thrust vectoring control technology[J]. Aeronautical Science and Technology, 1998(2):10-12(in Chinese).
[5]	BARHAM R W. Thrust vector aided maneuvering YF-22 advanced tactical fighter prototype:AIAA-1994-2105[R]. Reston, VA:AIAA, 1994.
[6]	TSENG J B, LAN C E. Aerodynamics of thrust vectoring by Navier-Stokes solutions:NASA Grant NAG 1-837[R]. Washington, D.C.:NASA, 1991.
[7]	李栋, 焦予秦, 宋科. 喷流-外流干扰流场数值模拟[J]. 航空学报, 2008, 29(2):292-296. LI D, JIAO Y Q, SONG K. Numerical simulation of external flow interfered by jet flow[J]. Acta Aeronautica et Astronautica Sinica, 2008, 29(2):292-296(in Chinese).
[8]	SHEU W L, LAN C E. Experimental investigation of the effect of thrust vectoring on lateral-directional aerodynamics at high angles of attack:AIAA-1994-1809[R]. Reston, VA:AIAA, 1994.
[9]	WANG Z J, JIANG P, GURSUL I. Effect of thrust-vectoring jets on delta wing aerodynamics[J]. Journal of Aircraft, 2007, 44(6):1877-1888.
[10]	DENG X Y, WANG Y K. An experimental study of interactive behaviors between vectoring jet and main flows[C]//Aerospace Science Meeting of AIAA. Reston, VA:AIAA, 1998.
[11]	HITZEL S M, WEIDE E, TREMEL U. X-31A vector high angle of attack descent Euler and Navier-Stokes simulations of unsteady maneuvers[C]//Proceedings of 23rd International Congress of Aeronautical Sciences. Toronto:ICAS Press, 2002, 243:1-9.
[12]	WANG Y K, DENG X Y. Effects of vectoring jet on aerodynamic characteristics of aircraft[J]. Chinese Journal of Aeronautics, 1998, 11(2):81-87.
[13]	王晋军, 刘激瀛, 薛启智. 矢量喷流对65°三角翼前缘涡破裂的影响[J]. 流体力学实验与测量, 2000,14(3):61-65. WANG J J, LIU J Y, XUE Q Z. The effects of vectored jet on leading edge vortex breakdown of 65° delta wing[J]. Experiments and Measurements in Fluid Mechanics, 2000,14(3):61-65(in Chinese).
[14]	汤伟, 黄勇, 傅澔. 推力矢量对飞机大迎角动态气动特性的影响[J]. 航空学报, 2018, 39(4):121648. TANG W, HUANG Y, FU H. Effect of thrust vector on dynamic aerodynamic characteristics of aircraft at high angle of attack[J]. Acta Aeronautica et Astronautica Sinica, 2018, 39(4):121648(in Chinese).
[15]	司芳芳, 袁先旭, 李建强, 等. 推力转向喷流与高速主流干扰参数影响规律的数值模拟研究[J]. 空气动力学学报, 2012, 30(5):583-591. SI F F, YUAN X X, LI J Q, et al. The study of the parameters' infection between vectoring jet and high speed main flows interaction[J]. Acta Aerodynamica Sinica, 2012, 30(5):583-591(in Chinese).
[16]	MCWATERS M A. F-35 conventional model jet-effects testing methodology:AIAA-2015-2404[R]. Reston, VA:AIAA, 2015.
[17]	王延奎, 邓学蓥, 张祖庚. 矢量喷流下平尾偏转对飞机气动性能的影响[J].北京航空航天大学学报, 2003, 29(2):156-160. WANG Y K, DENG X Y, ZHANG Z G. Experimental investigation on effect of horizontal tail deflection on aerodynamic characteristics of aircraft under vectoring jet[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(2):156-160(in Chinese).
[18]	李建强, 李耀华, 郭旦平, 等. 2.4米跨声速风洞推力矢量试验技术[J]. 空气动力学学报, 2016, 34(1):20-26. LI J Q, LI Y H, GUO D P, et al. The thrust vectoring experiment technique in the 2.4 m×2.4 m transonic wind tunnel[J]. Acta Aerodynamica Sinica, 2016, 34(1):20-26(in Chinese).
[19]	高静, 李聪, 杨勇, 等. 低速风洞推力矢量试验背撑干扰特性试验研究[J]. 实验流体力学, 2005,19(3):10-13. GAO J, LI C, YANG Y, et al. Researches of dorsal support interference in low speed wind tunnel thrust vector test[J]. Journal of Experiments in Fluid Mechanics, 2005, 19(3):10-13(in Chinese).
[20]	贾毅, 郑芳, 黄浩, 等. 低速风洞推力矢量试验技术研究[J]. 实验流体力学, 2014, 28(6):92-97. JIA Y, ZHENG F, HUANG H, et al. Research on vectoring thrust test technology in low-speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2014, 28(6):92-97(in Chinese).
[21]	金长江, 范立钦, 周士林. 飞机飞行性能计算[M]. 北京:国防工业出版社,1983:200-216. JIN C J, FAN L Q, ZHOU S L. Flight performance calculation of aircraft[M]. Beijing:National Defense Industry Press, 1983:200-216(in Chinese).

Wind tunnel test of canard aircraft interactive behaviors between vectoring jet and ground effect

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References 21

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Shanjie XU, Hongqiang LYU, Zhongchen LIU, Yan LENG, Xuejun LIU. Data analysis of sonic boom test based on probability model [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626269-626269.
[2]	Fangcheng SHI, Zhenxun GAO, Yuyan TIAN, Chongwen JIANG, Tiantian WANG, Chun-Hian LEE. Large eddy simulation of ideally expanded supersonic jet noise [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626266-626266.
[3]	Zhongchen LIU, Zhansen QIAN, Xuefei LI, Yan LENG, Dapeng GUO. Wind tunnel test techniques for exhaust nozzle plume effects on near-field sonic boom [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 626952-626952.
[4]	Zeyong YIN, Yancheng YOU, Chengxiang ZHU, Jianfeng ZHU, Liaoni WU, Yue HUANG. Multi-ducted twin-turbines ejector-ramjet/scramjet combined cycle engine for hypersonic civil vehicles [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(2): 627181-627181.
[5]	Jun SHU, Dongguang XU, Zhirong HAN, Si LI, Xiong HUANG. Hybrid wing design of icing wind tunnel supercooled large droplet icing test [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(1): 627182-627182.
[6]	Zhengxue MA, Zhenbing LUO, Aihong ZHAO, Yan ZHOU, Wei XIE, Qiang LIU, Yinxin ZHU, Wenqiang PENG. Reverse jet characteristics of plasma synthetic jet in hypersonic flow field [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 192-203.
[7]	Yifeng HUANG, Shuhua ZENG, Zhongzheng JIANG, Weifang CHEN. Numerical study on high-altitude lateral jet based on nonlinear coupled constitutive relation [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 8-22.
[8]	Xudong ZHANG, Zheng LI, Hao DONG, Siyuan GAO, Zubi JI, Kaixin LI, Guanghui BAI. Drag reduction characteristics of opposing plasma synthetic jet in hypersonic flow [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 115-123.
[9]	Xiangrong JING, Pan CHENG, Zhenbing LUO, Tianxiang GAO, Yan ZHOU, Xiong DENG. Ice breaking characteristics and crack propagation law of arc discharge plasma actuator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 204-213.
[10]	Zheng LI, Cong XU, Jian ZHANG, Mengmeng LI, Yilei MA, Guanghui BAI. Reverse jet flow control by plasma synthetic jet actuator in high speed flow field [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(S2): 225-232.
[11]	FU Yang'aoxiao, DING Mingsong, LIU Qingzong, JIANG Tao, SHI Run, DONG Weizhong, GAO Tiesuo. Numerical study of hot jet interaction effect in divert control system [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 125941-125941.
[12]	LIU Chuanzhen, MENG Xufei, LIU Rongjian, BAI Peng. Experimental and numerical investigation of hypersonic performance of double swept waverider [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 126015-126015.
[13]	LI Jun, WANG Junfeng, ZHAO Yatian, LUO Shibin. Research on combinational configuration of spike and multi-jets in off-design regimes [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(9): 125949-125949.
[14]	QIN Chen, ZHANG Rongping, ZHANG Junlong, YUE Tingrui, WU Songling. Acoustic performance of an under-expanded supersonic jet with different impinging distances to an inclined plate [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 125857-125857.
[15]	LIU Rubing, WEI Wentao, LI Fei, LIN Qi. Working mechanism of air-supplemented plasma synthetic jet actuator [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(8): 125854-125854.