碟形飞行低速特性

王林林; 高 歌

碟形飞行低速特性

王林林,
高歌

北京航空航天大学航空发动机气动热力重点实验室, 北京 100191

详细信息

作者简介:
王林林(1982-),男,河南登封人,博士生,junjifeng@live.com.

中图分类号: V 211.7
计量
- 文章访问数: 4595
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- PDF下载量: 1422
- 被引次数: 0
出版历程
- 收稿日期: 2009-01-14
- 网络出版日期: 2010-02-28

Low speed characteristics of the saucer-shaped aircraft

Wang Linlin,
Gao Ge

National Key Laboratory on Aero-Engines, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 碟形飞行器是一种新颖的,采用翼身融合布局的飞行器.为获得碟形飞行器在低速条件下的总体特性,对其进行了风洞测力和动导数测量试验,结合稳定性分析和模型试飞研究了其总体性能.研究结果表明:碟形飞行器最大升阻比为12.2,失速迎角28°,全机纵向模态稳定,横航向滚转模态和荷兰滚模态稳定,螺旋模态发散,具有良好的飞行品质和综合性能.
- 空气动力学 /
- 飞行力学 /
- 稳定性 /
- 碟形飞行器
Abstract: The saucer-shaped aircraft is a novel aircraft adopting blend-wing-body configuration. The wind tunnel experiments, stability analysis and flying tests were conducted to investigate the aerodynamic characteristics and stability features of the saucer-shaped aircraft under low speed conditions. The results show that the highest lift to drag ratio is 12.2, the stall angle of attack is 28°. Meanwhile saucer-shaped aircraft has stable longitudinal mode, rollover mode and Dutch roll mode. The spiral mode is unstable. The saucer-shaped aircraft exhibits superior flight qualities and excellent comprehensive performances.
- aerodynamics /
- flight dynamics /
- stability /
- saucer-shaped aircraft

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参考文献(1)

[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] 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)  [5] Bowers P M.Unconventional aircraft [M].USA:TAB Books Inc,1984: 94-95  [6] 范立钦,周鼎义.飞机空气动力学[M].西安:西北工业大学出版社,1989:134-135,262-263 Fan Liqin,Zhou Dingyi.Flight dynamics[M].Xi’an: Northwestern Polytechnical University Press,1989:134-135,262-263(in Chinese) [7] Katz J,Byrne S.Stall resistance feature of lifting-body airplane configurations[J].Journal of Aircraft,1999,36 (2):471-474 [8] 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):18-21 Ma Songhui,Wu Chengfu,Chen Huaimin.Study on stability and manoeuvrability of flying wing aircraft[J].Flight Dynamics,2006,24(3):18-21(in Chinese) [9] 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 [10] Ralph P,William G L.Dynamics and control of tailless aircraft .AIAA-97-3776,1997 [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)

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