全部 标题 作者
关键词 摘要

OALib Journal期刊
ISSN: 2333-9721
费用:99美元

查看量下载量

相关文章

更多...

全升力飞行器流场诱导流动现象改善效果

, PP. 1337-1341

Full-Text   Cite this paper   Add to My Lib

Abstract:

碟形飞行器是一种小展弦比全升力飞行器,采用一种仿生的鱼鳍型小翼对绕碟形飞行器的诱导流动现象进行改善,削弱翼尖诱导旋涡,提高整机气动效率.应用高精度风洞试验和以该风洞试验数据为校验的数值模拟,对鱼鳍型小翼的作用进行了研究,从风洞试验和数值模拟两方面给出了评判.研究结果表明鱼鳍型小翼对碟形飞行器的诱导流动现象有较大的改善效果.

References

[1]  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
[2]  王林林,高歌.碟形飞行器纵向飞行品质[J].北京航空航天大学学报,2008,34(12):1388-1391 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)
[3]  王林林,高歌.碟形飞行器横航向飞行品质[J].北京航空航天大学学报,2009,35(7):856-859 Wang Linlin,Gao Ge.Lateral and directional flight qualities of the saucer-shaped aircraft[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(7):856-859(in Chinese)
[4]  王林林,高歌.碟形飞行低速特性[J].北京航空航天大学学报,2010, 36(2): 223-226 Wang Linlin,Gao Ge.Low speed characteristics of the saucer-shaped aircraft[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(2):223-226(in Chinese)
[5]  于军力,王林林,高歌.碟形升力体飞行器气动性能[J].北京航空航天大学学报,2010,36(2):198-201 Yu Junli,Wang Linlin,Gao Ge.Investigation of aerodynamic characteristics on saucer-shaped lifting-body[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(2):198-201(in Chinese)
[6]  Wang Linlin,Gao Ge.Stability features of the saucer-shaped blend-wing-body aircraft[J].Advanced Material Research,2013,712:1307-1311
[7]  于军力,王林林,高歌.碟形升力体飞行器气动性能[J].北京航空航天大学学报,2010,36(2):198-201 Yu Junli,Wang Linlin,Gao Ge.Investigation of aerodynamic characteristics on saucer-shaped lifting-body[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(2):198-201(in Chinese)
[8]  Peter M B.Unconventional aircraft [M].USA:TAB Books Inc,1984:94-95
[9]  Wang Linlin,Gao Ge.Stability features of the saucer-shaped blend-wing-body aircraft[J].Advanced Material Research,2013,712:1307-1311
[10]  Sargeant M A,Hynes T P.Stability of hybrid-wing-body type aircraft with centerbody leading edge carving[J].Journal of Aircraft,2010,47(3):970-974
[11]  Peter M B.Unconventional aircraft [M].USA:TAB Books Inc,1984:94-95
[12]  Sargeant M A,Hynes T P.Stability of hybrid-wing-body type aircraft with centerbody leading edge carving[J].Journal of Aircraft,2010,47(3):970-974
[13]  恽起麟.风洞实验[M].北京:国防工业出版社,2000: 40- 46 Yun Qilin.Wind tunnel testing[M].Beijing:National Defense Industry Press,2000:40-46(in Chinese)
[14]  恽起麟.风洞实验[M].北京:国防工业出版社,2000: 40- 46 Yun Qilin.Wind tunnel testing[M].Beijing:National Defense Industry Press,2000:40-46(in Chinese)
[15]  李为吉.飞机总体设计[M].西安:西北工业大学出版社,2005:38-42 Li Weiji.Aircraft design[M].Xi-an:Northwestern Polytechnical University Press,2005:38-42 (in Chinese)
[16]  Menter F R.Two-equation eddy-viscosity turbulence models for engineering application [J].AIAA Journal,1994,32(8): 1598- 1605
[17]  李为吉.飞机总体设计[M].西安:西北工业大学出版社,2005:38-42 Li Weiji.Aircraft design[M].Xi-an:Northwestern Polytechnical University Press,2005:38-42 (in Chinese)
[18]  Menter F R.Two-equation eddy-viscosity turbulence models for engineering application [J].AIAA Journal,1994,32(8): 1598- 1605
[19]  吴光辉,陈迎春,顾诵芬.大型客机计算流体力学应用与发展[M].上海:上海交通大学出版社,2009:35-43 Wu Guanghui,Chen Yingchun,Gu Songfen.The applacation and development of CFD in large civil aircraft[M].Shanghai:Shanghai Jiaotong University Press,2009:35-43(in Chinese)
[20]  吴光辉,陈迎春,顾诵芬.大型客机计算流体力学应用与发展[M].上海:上海交通大学出版社,2009:35-43 Wu Guanghui,Chen Yingchun,Gu Songfen.The applacation and development of CFD in large civil aircraft[M].Shanghai:Shanghai Jiaotong University Press,2009:35-43(in Chinese)
[21]  Guo Chuanliang,Kipouros T.On the effects of turbulence modeling in design optimization for high-lift devices[R].AIAA-2012-1424,2012
[22]  Guo Chuanliang,Kipouros T.On the effects of turbulence modeling in design optimization for high-lift devices[R].AIAA-2012-1424,2012
[23]  Wood R M.The contributions of vincent justus burnelli .AIAA-2003-0292,2003
[24]  Wood R M.The contributions of vincent justus burnelli .AIAA-2003-0292,2003
[25]  Vos R,Dommelen J V.A conceptual and design and optimization method for Blend-Wing-Body aircraft .AIAA-2012-1756,2012
[26]  Vos R,Dommelen J V.A conceptual and design and optimization method for Blend-Wing-Body aircraft .AIAA-2012-1756,2012
[27]  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
[28]  王林林,高歌.碟形飞行器纵向飞行品质[J].北京航空航天大学学报,2008,34(12):1388-1391 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)
[29]  王林林,高歌.碟形飞行器横航向飞行品质[J].北京航空航天大学学报,2009,35(7):856-859 Wang Linlin,Gao Ge.Lateral and directional flight qualities of the saucer-shaped aircraft[J].Journal of Beijing University of Aeronautics and Astronautics,2009,35(7):856-859(in Chinese)
[30]  王林林,高歌.碟形飞行低速特性[J].北京航空航天大学学报,2010, 36(2): 223-226 Wang Linlin,Gao Ge.Low speed characteristics of the saucer-shaped aircraft[J].Journal of Beijing University of Aeronautics and Astronautics,2010,36(2):223-226(in Chinese)

Full-Text

Contact Us

service@oalib.com

QQ:3279437679

WhatsApp +8615387084133