ACTA AERONAUTICAET ASTRONAUTICA SINICA >
Numerical investigation into flow characteristics of tandem fan-wing configuration
Received date: 2015-10-23
Revised date: 2015-12-10
Online published: 2016-01-25
Fan-wing can accelerate and rectify the air inflow through the rapid rotation of crow flow fan in the leading edge. Taking advantage of this distinguishing feature, a tandem fan-wing configuration is put forward, which is composed by double or multiple rows of fan-wings arranged in tandem with certain spacing and spatial distribution. The flow characteristics of the tandem fan-wing configuration are simulated based on two dimensional models, and the lift and thrust loads are calculated for different spacing, height disparities and row numbers. Results indicate that compared to single fan-wing, larger lift and thrust can be obtained by properly designed tandem fan-wing configuration. For instance, the four-row fan-wing with uniform spacing of one fan diameter possesses larger average lift and thrust by about 10% and 30%,respectively. The reason accounting for the improvement of lift and thrust is analyzed based on the flow filed near the fan-wings and the pressure distribution over the airfoils. These investigations can provide useful guidance for the design of future fan-wing aircraft with better low-speed large-load characteristics.
Key words: fan-wing; aerodynamic configuration; flow characteristics; spacing; row number
SHI Zhenhai , YANG Weizhu , LU Xiuru , YUE Zhufeng . Numerical investigation into flow characteristics of tandem fan-wing configuration[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2016 , 37(10) : 2922 -2931 . DOI: 10.7527/S1000-6893.2015.0356
[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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