Citation: | Liu Peiqing, Kuang Jianmin, Qu Qiulinet al. Effect and mechanism of lift-enhancement of the co-flow jet technology[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(6): 737-740. (in Chinese) |
[1] Cichy D R, Harris J W, Mackay J K. Flight test of a rotating cylinder flap on a North American Rockwell YOV-10 aircraft . NASA CR-2135, 1972 [2] Modi V J, Fernando M, Yokomizo T. Drag reduction of bluff bodies through moving surface boundary layer control . AIAA-90-0298, 1990 [3] 刘宝杰,杨晓宁,沈遐龄,等.几种前缘流动控制的实验研究[J].工程热物理学报, 1998, 19(4): 444-448 Liu Baojie, Yang Xiaoning, Shen Xialing, et al. Experimental investigation of separation flow control using vortex-generating devices[J].Journal of Engineering Thermophysics, 1998, 19(4): 444-448 (in Chinese) [4] Wood N J, Roberts L. Control of vortical lift on delta wings by tangential leading-edge blowing[J]. Journal of Aircraft, 1988, 25(3): 236-243 [5] Wood N J, Nielsen J N. Circulation control airfoil-past, present, future . AIAA-85-0204, 1985 [6] Englar R J. Circulation control for high lift and drag generation on STOL aircraft[J]. Journal of Aircraft, 1975, 12(5): 457-463 [7] Zha G C, Paxton C. A novel airfoil circulation augment flow control method using co-flow jet . AIAA-2004-2208, 2004 [8] Paxton C, Zha G C. Design of the secondary flow system for a co-flow jet cascade . AIAA-2004-3928, 2004 [9] Zha G C, Carroll B F, Paxton C, et al. High performance airfoil using co-flow jet flow control . AIAA-2005-1260, 2005 [10] 《航空气动力手册》编写组.航空气动力手册第二册[M].北京:国防工业出版社, 1983: 384 Aeronautical Aerodynamics Manual Editor Group. Aeronautical aerodynamics manual volume 2[M].Beijing:National Defense Industry Press, 1983: 384 (in Chinese)
|