Citation: | Wang Linlin, Gao Ge. Longitudinal flight qualities of the saucer-shaped aircraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2008, 34(12): 1388-1391. (in Chinese) |
[1] Liebeck R H. Design of the blended-wing-body subsonic transport .AIAA-02-13493, 2002 [2] Ricketts R H,Noll T E, Woodrow W J,et al. An overview of aeroelasticity studies for the national aero-space plane . AIAA-93-1313-CP, 1993 [3] Murphy K J,Nowak R J,Thompson R A, et al. X-33 hypersonic aerodynamic characteristics . AIAA-99-4162, 1999 [4] Yu Junli,Wang Linlin,Gao Ge. Using wing tip devices to improve performance of saucer-shaped aircraft[J].Chinese Journal of Aeronautics, 2006,19(4):309-314 [5] 李晓勇,张淼,鲁素芬,等.翼身融合飞机的空气动力学研究进展[J].飞机设计,2007,27(2):1-2 Li Xiaoyong,Zhang Miao,Lu Sufeng, et al. Advances in aerodynamics for blended-wing-body aircraft[J].Aircraft Desin,2007,27(2):1-2(in Chinese) [6] Kresse N. Challenges and potential of BWB configuration (results of the projects VELA-very large aircraft) . Fifth Community Aeronautical Days 2006, 2006 [7] Gibson C S,Vess R J,Pegg R.Low speed testing of an X-43A hypersonic lifting body configuration . AIAA-03-7086,2003 [8] Mras P J,Humphreys D E,Langehough M A.DarkStar flight control system design . Association for Unmanned Vehicle Systems International Annual Symposium Exhibition, 1999 [9] 马松辉,吴成富,陈怀民.飞翼飞机稳定性与操作性研究[J].飞行力学,2006,24(3):18-19 Ma Songhui,Wu Chengfu,Chen Huaimin.Study on stability and manoeuvrability of flying wing aircraft[J].Flight Dynamics, 2006,24(3):18-19(in Chinese) [10] 吴森堂,费玉华.飞行控制系统[M].北京:北京航空航天大学出版社,2005:73-88 Wu Sentang,Fei Yuhua.Flight control systems[M].Beijing: Beijing University of Aeronautics and Astronautics Press,2005:73-88(in Chinese) [11] GJB185-86.有人驾驶飞机(固定翼)飞行品质 [S] GJB185-86.Flying qualities of piloted planes (fixed wings) [S](in Chinese) [12] 王劲东,沈遐龄,高歌.碟形升力体的低速特性研究[J].北京航空航天大学学报,2003,29(4):346-349 Wang Jindong,Shen Xialing,Gao Ge.Experimental research of low speed aerodynamic characteristics of saucer-like lifting body[J].Journal of Beijing University of Aeronautics and Astronautics,2003,29(4):346-349(in Chinese)
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