| Citation: | YANG Kelong, HAN Dong, SHI Qipeng. Lifting and propulsion devices for flight performance ,improvement of a compound helicopter[J]. Journal of Aerospace Power, 2020, 35(11): 2429-2439. doi: 10.13224/j.cnki.jasp.2020.11.020
|
| [1] |
COLUCCI F.Compound interest［J］.Vertifilite,2001,47(2):24-27.
|
| [2] |
COLUCCI F.Speed hawk-phase I［J］.Vertifilite,2007,53(4):18-22.
|
| [3] |
HIESCHBERG M.Sikorsky pushers forward with X2 technology demonstrator［J］.Vertifilite,2005,51(3):12-14.
|
| [4] |
WALSH D,WEINER S,ARIFIAN K,et al.High airspeed testing of the sikorsky X2 technology demonstrator［C］∥67th Annual Forum Proceedings of the American Helicopter Society.Virginia Beach,USA:Vertical Flight Society,2011:2999-3010.
|
| [5] |
HIESCHBERG M.X2,X3,S-97 and X-49:the battle of the compounds is joined［J］.Vertifilite,2010,56(4):16-22.
|
| [6] |
ORCHARD M,NEWMAN S.The fundamental configuration and design of the compound helicopter［J］.Journal of Aerospace Engineering,2003,217(6):297-315.
|
| [7] |
FLOROS M W,JOHNOSN W R.Performance analysis of the slowed-rotor compound helicopter configuration［J］.Journal of the American Helicopter Society,2009,54(2):1-12.
|
| [8] |
RAND O,KHROMOV V.Compound helicopter:insight and optimization［J］.Journal of the American Helicopter Society,2015,60(1):1-12.
|
| [9] |
BOWEN G,YEO H.Performance and loads study of a high-speed compound helicopter［J］.Journal of the American Helicopter Society,2018,63(3):20-34.
|
| [10] |
YEO H.Design and aeromechanics investigation of compound helicopters［R］.Jeju Island,Korea:Vertical Flight Society,2018.
|
| [11] |
邓艳敏,陶然,胡继忠.共轴式直升机上下旋翼之间气动干扰的风洞实验研究［J］.航空学报,2003,24(1):10-14. DENG Yanmin,TAO Ran,HU Jizhong.Experimental investigation of the aerodynamic interaction between upper and lower rotors of a coaxial helicopter［J］.Acta Aeronautica et Astronautica Sinica,2003,24(1):10-14.(in Chinese)
|
| [12] |
万佳,陈铭.复合式直升机前飞状态旋翼-机翼干扰计算分析［J］.航空动力学报,2009,24(11):2459-2464. WAN Jia,CHEN Ming.Rotor-wing interaction analysis of a compound helicopter in forward flight［J］.Journal of Aerospace Power,2009,24(11):2459-2464.(in Chinese)
|
| [13] |
李建波.复合式直升机技术发展分析［J］.南京航空航天大学学报,2016,48(2):149-158. LI Jianbo.Analysis of technology development of compound helicopter［J］.Journal of Nanjing University of Aeronautics and Astronautics,2016,48(2):149-158.(in Chinese)
|
| [14] |
曹飞,陈铭.一种单旋翼复合式直升机性能特性［J］.北京航空航天大学学报,2016,42(4):772-779. CAO Fei,CHEN Ming.Performance characteristics of single rotor compound helicopter［J］.Journal of Beijing University of Aeronautics and Astronautics,2016,42(4):772-779.(in Chinese)
|
| [15] |
PETERS D A,HAQUANG,N.Dynamic inflow for practical application［J］.Journal of the American Helicopter Society,1988,33(4):64-68.
|
| [16] |
韩东.变转速旋翼直升机性能及配平研究［J］.航空学报,2013,34(6):1241-1248. HAN Dong.Study on the performance and trim of helicopters with variable speed rotors［J］.Acta Aeronautica et Astronautica Sinica,2013,34(6):1241-1248.(in Chinese)
|
| [17] |
董晨,韩东,杨克龙.独立桨距控制对直升机飞行性能的影响［J］.航空学报,2018,39(10):1241-1248. DONG Chen,HAN Dong,YANG Kelong.Effect of individual blade pitch control on flight performance of helicopters［J］.Acta Aeronautica et Astronautica Sinica,2018,39(10):1241-1248.(in Chinese)
|
| [18] |
FELKER F F,LIGHT J S.Aerodynamic interactions between a rotor and wing in hover［J］.Journal of the American Helicopter Society,1986,33(2):64-68.
|
| [19] |
PASSE B J,SRIDHARAN A,BAEDER J D.Computational investigation of coaxial rotor interactional aerodynamics in steady forward flight［R］.AIAA 2015-2883,2015.
|
| [20] |
KIM H W,KENYON A R,BROWN R E.Interactional aerodynamics and acoustics of a hingeless coaxial helicopter with an auxiliary propeller in forward flight［J］.Aeronautical Journal,2008,113(1140):65-78.
|
| [21] |
GUDMUNDSSON S.General aviation aircraft design［M］.Oxford,UK:Butterworth-Heinemann Press,2013.
|
| [22] |
刘沛清.空气螺旋桨理论及其应用［M］.北京:北京航空航天大学出版社,2006.
|
| [23] |
LEISHMAN J G.Principles of helicopter aerodynamics［M］.New York:Cambridge University Press,2006.
|
| [24] |
HILBERT K B.A mathematical model of the UH-60 helicopter［R］.NASA-TM-85890,1984.
|
| [25] |
DAVIS S J.Predesign study for a modern 4-bladed rotor for the RSRA［R］.NASA-TM-166155,1981.
|
| [26] |
BOUSMAN W.Aerodynamic characteristics of SC1095 and 1094R8 airfoils［R］.NASA-TP-212265,2003.
|
| [27] |
YEO H,BOUSMAN W,JOHNSON W R.Performance analysis of a utility helicopter with standard and advanced rotors［J］.Journal of the American Helicopter Society,2004,49(3):250-270.
|
| [28] |
SIVELLS J C.Experimental and calculated characteristics of three wings of NACA 64-210 and 65-210 airfoil Sections with and without 2 degree washout［R］.NASA-TP-1422,1947.
|
| [29] |
SANTOS P D.Aero-structural wing analysis using a vortex,lattice method coupled with an equivalent plate model［D］.Covilha,Portugal:University of the Interior Border Engineering,2011.
|
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