| [1] DANG T Q, BUSHNELL P R. Aerodynamics of cross-flow fans and their application to aircraft propulsion and flow control[J]. Progress in Aerospace Sciences, 2009, 45(1):1-29.
[2] THOUAULT N, BREITSAMTER C, ADAMS N A. Numerical and experimental analysis of a generic fan-in-wing configuration[J]. Journal of Aircraft, 2009, 46(2):656-666.
[3] DYGERT R K, DANG T Q. Experimental investigation of embedded crossflow fan for airfoil propulsion/circulation control[J]. Journal of Propulsion and Power, 2009, 25(1):196-203.
[4] GOHARDANI A S, DOULGERIS G, SINGH R. Challenges of future aircraft propulsion:A review of distributed propulsion technology and its potential application for the all electric commercial aircraft[J]. Progress in Aerospace Sciences, 2011, 47(5):369-391.
[5] PEEBLES P. Aerodynamic lift generating device:US Patent 6527229B1[P]. 2003-03-04.
[6] SEYFANG G R. Recent developments of the fan-wing aircraft[C]//The 3rd CEAS Air & Space Conference. Venice:Council of European Aerospace Societies, 2011:1-7.
[7] 孟琳, 叶永强, 李楠. 扇翼飞行器的研究进展与应用前景[J]. 航空学报, 2015, 36(8):2651-2661. MENG L, YE Y Q, LI N. Research progress and application prospects of the fan-wing aircraft[J]. Acta Aeronautica et Astronautica Sinica, 2015, 36(8):2651-2661(in Chinese).
[8] FORSHAW S. Wind tunnel investigation of new fan wing design[D]. London:Imperial College, 1999:10-25.
[9] KOGLER K U. Fanwing, experimental evaluation of a novel lift & propulsion device[D]. London:Imperial College, 2002:21-40.
[10] AHAD O, GRAHAM J M R. Flight simulation and testing of the FanWing experimental aircraft[J]. Aircraft Engineering and Aerospace Technology, 2007, 79(2):131-136.
[11] ASKARI S, SHOJAEEFARD M H. Numerical simulation of flow over an airfoil with a cross flow fan as a lift generating member in a new aircraft model[J]. Aircraft Engineering and Aerospace Technology, 2009, 81(1):59-64.
[12] ASKARI S, SHOJAEEFARD M H. Experimental and numerical study of an airfoil in combination with a cross flow fan[J]. Proceedings of the Institution of Mechanical Engineers, Part G:Journal of Aerospace Engineering, 2013, 227(7):1173-1187.
[13] 吴浩东. 风扇翼内部偏心涡特性研究[D]. 南京:南京航空航天大学, 2012:1-75. WU H D. Research on the characteristic of the eccentric vortex in the fan-wing[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012:1-75(in Chinese).
[14] DUDDEMPUDI D, YAO Y, EDMONDSON D, et al. Computational study of flow over generic fan-wing airfoil[J]. Aircraft Engineering and Aerospace Technology, 2007, 79(3):238-244.
[15] ASKARI S, SHOJAEEFARD M H. Shape optimization of the airfoil comprising a cross flow fan[J]. Aircraft Engineering and Aerospace Technology, 2009, 81(5):407-415.
[16] 蒋甲利, 牛中国, 刘捷, 等. 扇翼飞行器机翼布局研究[J]. 航空科学技术, 2009(3):30-35. JIANG J L, NIU Z G, LIU J, et al. Research on the wing composition of fan-wing aircraft[J]. Aeronautical Science and Technology, 2009(3):30-35(in Chinese).
[17] 唐荣培. 风扇翼气动特性试验研究[D]. 南京:南京航空航天大学, 2014:1-74. TANG R P. Experimental study on the aerodynamic characteristics of the fan-wing[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2014:1-74(in Chinese).
[18] 张银辉. 风扇翼非定常流动的数值分析[D]. 南京:南京航空航天大学, 2012:49-61. ZHANG Y H. Numerical analysis on unsteady characteristics of the fan-wing flow field[D]. Nanjing:Nanjing University of Aeronautics and Astronautics, 2012:49-61(in Chinese).
[19] 芦志明, 冯衬, 唐正飞. 扇翼三维几何参数对气动性能影响分析[J]. 军民两用技术与产品, 2015(4):173-175. LU Z M, FENG C, TANG Z F. The analysis of three-dimensional geometric model fan-wing parameters impact to aerodynamic performance[J]. Dual Use Technologies & Products, 2015(4):173-175(in Chinese).
[20] SEYFANG G R. Fanwing-developments and applications[C]//The 28th International Congress of the Aeronautical Sciences. Brisbane:International Council of the Aeronautical Sciences, 2012:238-246. |
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