[1] 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 D. Study on the performance and trim of helicopters with variable speed rotors[J]. Acta Aeronoutica et Astronautica Sinica, 2013, 34(6):1241-1248(in Chinese).
[2] KANG H. Dynamic blade shape for improved helicopter rotor performance[J]. Journal of the American Helicopter Society, 2010, 55(3):32008-1-11.
[3] 韩东, 林长亮, 李建波. 旋翼变体技术对直升机性能的提升[J]. 航空动力学报, 2014, 29(9):2017-2023. HAN D, LIN C L, LI J B. Helicopter performance improvement by rotor morphing technologies[J]. Journal of Aerospace Power, 2014, 29(9):2017-2023(in Chinese).
[4] 韩东, 张勇刚, 黄东盛. 变直径旋翼直升机飞行性能研究[J]. 南京航空航天大学学报, 2015, 47(2):252-258. HAN D, ZHANG Y G, HUANG D S. Helicopter flight performance improvement by variable rotor diameter[J]. Journal of Nanjing University of Aeronautics & Astronautics, 2015, 47(2):252-258(in Chinese).
[5] LIEBECK R H. Design of subsonic airfoils for high lift[J]. Journal of Aircraft, 1978, 15(9):547-561.
[6] NEUHART D H, PENDERGRAFT O C. A water tunnel study of Gurney flaps:NASA-TM-4071[R]. Washington, D.C.:NASA Langley Research Center, 1988.
[7] JEFFREY D, ZHANG X. Aerodynamics of Gurney flaps on a single-element high-lift wing[J]. Journal of Aircraft, 2000, 37(2):295-301.
[8] JEFFREY D R M, HURST D W. Aerodynamics of the Gurney flap[C]//Proceedings of the 14th AIAA Applied Aerodynamics Conference. Reston:AIAA,1996:349-358.
[9] CAMOCARDI M E, LEO J M D, DELNERO J S, et al. Experimental study of a NACA4412 airfoil with movable Gurney flap[C]//Proceedings of the 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition. Reston:AIAA, 2011:1-15.
[10] LI Y C, WANG J J, ZHANG P F. Influences of mounting angles and locations on the effects of Gurney flaps[J]. Journal of Aircraft, 2003, 40(3):494-498.
[11] YEE K, JOO W, LEE D H. Aerodynamic performance analysis of a Gurney flap for rotorcraft application[J]. Journal of Aircraft, 2007, 44(3):1003-1014.
[12] MYOSE R, HERON I, PAPADAKIS M. The post-stall effect of Gurney flaps on a NACA 0011 airfoil[J]. American Technical Publishers LTD, 1996, 105(1):173-178.
[13] 崔钊, 韩东, 李建波. 翼型加装格尼襟翼的高亚声速气动特性研究[J]. 航空学报, 2013, 34(10):2277-2286. CUI Z, HAN D, LI J B. Study on aerodynamic characteristics of airfoil with Gurney flaps under high subsonic flow[J]. Acta Aeronoutica et Astronautica Sinica, 2013, 34(10):2277-2286(in Chinese).
[14] 崔钊, 李建波, 赵洪. 翼型加装格尼襟翼的低雷诺数气动特性实验研究[J]. 实验流体力学, 2013, 27(4):1-6. CUI Z, LI J B, ZHAO H. Experimental study on aerodynamic characteristics of airfoil equipped with Gurney flaps at low reynolds numbers[J]. Journal of Experiments in Fluid Mechanics, 2013, 27(4):1-6(in Chinese).
[15] 崔钊, 韩东, 李建波, 等. 加装格尼襟翼的自转旋翼气动特性研究[J]. 航空学报, 2012, 33(10):1791-1799. CUI Z, HAN D, LI J B, et al. Study on aerodynamic characteristics of auto-rotating rotors with Gurney flaps[J]. Acta Aeronoutica et Astronautica Sinica, 2012, 33(10):1791-1799(in Chinese).
[16] MIN B Y, SANKAR L N, RAJMOHAN N et al. Computational investigation of the effects of Gurney flap on forward flight characteristics of helicopter rotors[J]. Journal of Aircraft, 2009, 46(6):1957-1964.
[17] LEISHMAN J G. Principles of helicopter aerodynamics[M]. New York:Cambridge University Press, 2006:171-209.
[18] PETERS D A, HAQUANG N. Dynamic inflow for practical applications[J]. Journal of the American Helicopter Society, 1988, 33(4):64-68.
[19] KENTFIELD J A C. The potential of Gurney flaps for improving the aerodynamic performance of helicopter rotors[C]//International Powered Lift Conference. Reston:AIAA, 1993:283-292.
[20] TRAUB L W, MILLER A C, REDINIOTIS O. Preliminary parametric study of Gurney-flap dependencies[J]. Journal of Aircraft, 2006, 43(4):1242-1244.
[21] WANG J J, LI Y C, CHOI K S. Gurney flap-lift enhancement mechanisms and applications[J]. Progress in Aerospace Sciences, 2008, 44(1):22-47.
[22] HILBERT K B. A mathematical model of the UH-60 helicopter:NASA-TM-85890[R]. Moffett Field:Aeromechanics Laboratory, US Army Research and Technology Laboratories-AVSCOM Ames Research Center, 1984:11-24.
[23] YEO H, BOUSMAN W G, JOHNSON W. Performance analysis of a utility helicopter with standard and advanced rotors[J]. Journal of the American Helicopter Society, 2004, 49(3):250-270. |