Thiel M. Actuation of an active Gurney flap for rotorcraft applications. University Park: The Pennsylvania State University, 2006.
[2]
Li Y C, Wang J J, Fan J C, et al. Experiment investigation into effects of Gurney flaps on supercritical airfoil. Journal of Beijing University of Aeronautics and Astronautics, 2003, 29(6): 471-474. (in Chinese) 李亚臣, 王晋军, 樊建超, 等. 超临界翼型Gurney襟翼增升试验研究. 北京航空航天大学学报, 2003, 29(6): 471-474.
[3]
Zhou H. Numerical analysis of effect of mini-TED on aerodynamic characteristics of airfoils in transonic flow. Acta Aeronautica et Astronuatica Sinica, 2009, 30(8): 1367-1373. (in Chinese) 周华. Mini-TED改变翼型跨声速性能的数值分析. 航空学报, 2009, 30(8): 1367-1373.
[4]
Stivers L S, Rice F J. Aerodynamic characteristics of four NACA airfoil sections designed for helicopter rotor blades.NACA RB No.l5k02, 1946.
[5]
Schaefer R, Smith H. Aerodynamic characteristics of the NACA 8-H-12 airfoil section at six Reynolds numbers from 1.8×106 to 11.0×106. NACA TN 1998, 1998.
[6]
Menter F. Two-equation eddy viscosity turbulence models for engineering applications. AIAA Journal, 1994, 32(8): 1598-1605.
[7]
Cook P H, McDonald M A, Firmin M C P. Aerofoil RAE 2822-pressure distributions and boundary layer and wake measurements. AGARD Report AR 138, 1979: A6.
[8]
Liebeck R H. Design of subsonic airfoils for high lift. Journal of Aircraft, 1978, 15(9): 547-561.
[9]
Neuhart D H, Pendergraft O C. A water tunnel study of Gurney flaps. NASA TM 4071, 1988.
[10]
Storms B L, Jang C S. Lift enhancement of an airfoil using a Gurney flap and vortex generators. Journal of Aircraft, 1994, 31(3): 542-547.
[11]
Jang C S, Ross J C, Cummings R M. Computational evaluation of an airfoil with a Gurney flap. AIAA-1992-2708, 1992.
[12]
Myose R, Heron I, Papadakis M. The effect of Gurney flaps on a NACA 0011 airfoil. AIAA-1996-59, 1996.
[13]
Myose R, Heron I, Papadakis M. The post-stall effect of Gurney flaps on a NACA 0011 airfoil. SAE Technical Paper 961316, 1996.
[14]
Lee H T, Kroo I M. Computational investigation of wings with miniature trailing edge control surfaces. AIAA-2004-2693, 2004.
[15]
Li Y C, Wang J J. Experimental investigation of Gurney flaps on the lift enhancement of a delta wing. Acta Aerodynamica Sinica, 2002, 20(4): 388-393. (in Chinese) 李亚臣, 王晋军. 三角翼Gurney襟翼增升实验研究. 空气动力学报, 2002, 20(4): 388-393.
[16]
Gao Y W. Method using Gurney flap to increase flux of an axial fan. Fluid Machinery, 2004, 32(1): 18-20. (in Chinese) 高永卫. Gurney襟翼在车辆冷却风扇设计中的应用研究. 流体机械, 2004, 32(1): 18-20.
[17]
Shen Z H, Yu G L. Experimental investigation of effect of Gurney flap on performance of horizontal-axis wind turbine. Acta Energiae Solaris Sinica, 2007, 28(2): 196-199. (in Chinese) 申振华, 于国亮. Gurney襟翼对水平轴风力机性能影响的实验研究. 太阳能学报, 2007, 28(2): 196-199.
[18]
Min B Y, Sankar L N, Rajmohan N. Computational investigation of the effects of Gurney flap on forward flight characteristics of helicopter rotors. Journal of Aircraft, 2009, 46(6): 1957-1964.
[19]
Yeo H. Assessment of active controls for rotor performance enhancement. Journal of the American Helicopter Society, 2008, 53(2): 152-163.
[20]
Bae S, Gandhi F, Maughmer M. Optimally scheduled deployment of Gurney flaps for rotorcraft power reduction. Proceedings of the 65th Annual Forum of the American Helicopter Society, 2009: 187-211.
[21]
Kinzel M, Maughmer M, Lesieutre G. Miniature trailing-edge effectors for rotorcraft performance enhancements. Journal of the American Helicopter Society, 2007, 52(2):146-158.
