倾转旋翼机旋翼/机翼气动干扰理论与试验

doi:10.7527/S1000-6893.2016.0228

Abstract

Abstract:

A new model for rotor/wing aero-interaction in tilt-rotor aircraft is established by parametirc modeling method, which suits to flight dynamic analysis. The expression for calculating the boundary of rotor/wing aero-interaction area is derived using a simple and accurate method. The area of interaction is then calculated with analytical expression of numerical integration, as well as the velocity boundary of rotor/wing interaction. A wing tunnel test for tilt-rotor is conducted in different rotor collective pitch, wind velocity and nacelle angle. The comparison between test and calculation shows the effectiveness of this new model.

Key words: tilt-rotor aircraft, aero-interaction, interaction boundary, analytical expression, wind tunnel test

CLC Number:

V212.4

ZHANG Zheng, CHEN Renliang. Theory and test of rotor/wing aero-interaction in tilt-rotor aircraft[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(3): 120196-120196.

References

[1] 李鹏, 招启军. 悬停状态倾转旋翼/机翼干扰流场及气动力的CFD计算[J]. 航空学报, 2014, 35(2):361-371. LI P, ZHAO Q J. CFD calculations on the interaction flow field and aero-dynamic force of tilt-rotor/wing in hover[J]. Acta Aeronautica et Astronautica Sinica, 2014, 35(2):361-371(in Chinese).
[2] 徐恺. 倾转旋翼飞行器旋翼/机翼/机身气动干扰计算[D]. 南京:南京航空航天大学, 2007. XU K. Calculation of aerodynamic interaction between rotor/wing/fuselage of tilt-rotor[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2007(in Chinese).
[3] GEORGE F I. Navier-Stokes flowfield computation of wing/rotor interaction for a tilt rotor aircraft in hover[D]. Palo Alto:Stanford University, 1992.
[4] 李春华, 黄水林, 徐国华. 倾转旋翼机机翼向下载荷的计算方法及参数影响分析[J]. 实验流体力学, 2007, 21(1):13-18. LI C H, HUANG S L, XU G H. Calculated method and parameter effect investigation of wing download of tiltrotor aircraft[J]. Journal of Experiments in Fluid Mechanics, 2007, 21(1):13-18(in Chinese).
[5] 沙虹伟. 无人倾转旋翼机飞行力学建模与姿态控制技术研究[D]. 南京:南京航空航天大学, 2007. SHA H W. A mathematical model of unmanned tiltrotor aircraft and research on attitude control system design[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2007(in Chinese).
[6] 沙虹伟, 陈仁良. 倾转旋翼机飞行力学特性[J]. 航空动力学报, 2014, 27(2):749-754. SHA H W, CHEN R L. Flight dynamic characteristic of tilt rotor aircraft[J]. Journal of Aerospace Power, 2012, 27(2):749-754(in Chinese).
[7] 宋彦国, 王焕瑾, 沙虹伟, 等. 倾转旋翼飞行器飞行力学模型研究[J]. 空气动力学学报, 2008, 26(2):192-196. SONG Y G, WANG H J, SHA H W, et al. Flight dynamic mathematical model of tiltrotor aircraft[J]. Acta Aerodynamics Sinica, 2008, 26(2):192-196(in Chinese).
[8] KLEINHESSELINK K M. Stability and control modeling of tiltrotor aircraft[D]. College Park:University of Maryland, 2007.
[9] 曹芸芸, 陈仁良. 倾转旋翼飞行器旋翼对机翼向下载荷计算模型[J]. 航空动力学报, 2011, 26(2):468-474. CAO Y Y, CHEN R L. Mathematical model for calculating wing download of tiltrotor aircraft[J]. Journal of Aerospace Power, 2011, 26(2):468-474(in Chinese).
[10] HAREMDRA P B, JOGLEKAR M J, CAFFEY T M, et al. A mathematical model for real time flight simulation of the Bell model 301 tilt rotor research aircraft:NASA-CR-114614[R]. Washington, D.C.:NASA, 1973.
[11] CARLSON E B, ZHAO Y Y, ROBERT T N. Optical tiltrotor runway operations in one engine inoperative:AIAA-1999-3961[R].Reston:AIAA,1999.
[12] CARLSON E B. Optical tiltrotor aircraft operations during power failure[D]. Bologna:University of Minnesota, 1999.
[13] 曹芸芸. 倾转旋翼飞行器飞行动力学数学建模方法研究[D].南京:南京航空航天大学, 2012. CAO Y Y. Research on mathematical modeling method for tilt rotor aircraft flight dynamic[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012(in Chinese).
[14] 杨喜立,朱纪洪,黄兴李,等. 倾转旋翼飞机建模与仿真[J].航空学报,2006,27(4):584-587. YANG X L, ZHU J H, HUANG X L, et al. Modeling and simulation for tilt rotor airplane[J]. Acta Aeronautica et Astronautica Sinica, 2006, 27(4):584-587(in Chinese).
[15] 张义涛,李明,李达. 倾转旋翼飞行器飞行仿真建模[J]. 直升机技术, 2008, 154(2):11-16. ZHANG Y T, LI M, LI D. A simplified flight simulation model of tilt rotor aircraft[J]. Helicopter Technique, 2008,154(2):11-16(in Chinese).
[16] 程尚. 倾转旋翼飞行器建模及仿真研究[D].南京:南京航空航天大学, 2010. CHENG S. Modelling and simulation of tiltrotor[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2010(in Chinese).
[17] CHURCHILL G B, DUGAN D C. Simulation of the XV-15 tilt rotor research aircraft:NASA TM-84222[R]. Washington, D.C.:NASA, 1982.
[18] JHEMI A A, CARLSON E B, ZHAO Y J. Optimization of rotorcraft flight following engine failure[J].Journal of the American Helicopter Society, 2004, 49(2):117-126.
[19] HEUZE O, DIAZ S, DESOPPER A. Simplified models for tiltrotor aerodynamic phenomena in hover and low speed flight[C]//Aerospace Aerodynamics Research Conference, 2002:1-11.
[20] 郭剑东. 无人倾转旋翼机飞行控制研究[D]. 南京:南京航空航天大学, 2013. GUO J D. Flight control of unmanned tiltrotor aircraft[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2013(in Chinese).
[21] 王适存. 直升机空气动力学[M]. 北京:航空专业教材编审组, 1985:13-14. WANG S C. Helicopter aerodynamics[M]. Beijing:Aviation Professional Editor Group, 1985:13-14(in Chinese).

Theory and test of rotor/wing aero-interaction in tilt-rotor aircraft

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

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]	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.
[3]	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.
[4]	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.
[5]	LIU Jun, LUO Xinfu, WANG Xiansheng. Experiment on influence of leading-edge shape on aerodynamic characteristics of cavity model [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(7): 125235-125235.
[6]	ZHANG Zhenkai, JIA Sijia, SONG Chen, YANG Chao. Optimum design of wind tunnel test model for compliant morphing trailing edge [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 226071-226071.
[7]	HOU Yingyu, LI Qi, JI Chen, LIU Ziqiang. Experimental design of aeroelastic load with supersonic low frequency and large buffeting [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(3): 626454-626454.
[8]	ZENG Kaichun, KOU Xiping, YANG Xinghua, YU Li, ZHA Jun. Optimization of active vibration damping structure for transonic wind tunnel test model [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(2): 224944-224944.
[9]	LIU Jiahao, LI Gaohua, WANG Fuxin. Rotor-wing aerodynamic interference characteristics in conversion mode [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(12): 126097-126097.
[10]	YI Bingli, LIU Boyu, WANG Zhengqu, ZHANG Tiejun, LU Dan, ZHAO Yan. Test technology of twin-sting supports in 1.2 m high speed wind tunnel [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526794-526794.
[11]	JIANG Youxu, LI Jie, YANG Zhao. Data correction method of wind tunnel test for verification aircraft with laminar wing section [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526814-526814.
[12]	WANG Meng, LI Yujun, ZHAO Ronghuan, ZHONG Hongjie. Transition detection technique for wide speed range by means of on-line heating coating [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526820-526820.
[13]	ZHOU Zhenyao, LYU Fei, ZHOU Bin, YANG Zhao. Verification method for natural laminar flow drag reduction and layout design of test section [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526751-526751.
[14]	LI Qian, WANG Yankui, JIA Yuhong. Roll oscillations over wing-body configuration with strake wings: Experiment [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526008-526008.
[15]	WANG Hao, ZHONG Min, HUA Jun, ZHONG Hai, YANG Tihao, WANG Meng, LEI Guodong. Simulation and experiment of natural laminar flow flight test wing glove [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2022, 43(11): 526785-526785.