浮升混合飞艇气动性能及总体参数分析

糜攀攀; 孟军辉; 吕明云

doi:10.13700/j.bh.1001-5965.2014.0404

浮升混合飞艇气动性能及总体参数分析

doi: 10.13700/j.bh.1001-5965.2014.0404

北京航空航天大学航空科学与工程学院, 北京 100191

基金项目: 航空科学基金(2012ZA51009)

详细信息

作者简介:
糜攀攀(1989—),男,四川达州人,硕士研究生,BluceMi@163.com

通讯作者:
吕明云(1969—),男,湖北公安人,教授,lv503@buaa.edu.cn,主要研究方向为飞行器总体设计、飞行器隐身技术.

中图分类号: V274
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- 被引次数: 0
出版历程
- 收稿日期: 2014-07-04
- 网络出版日期: 2015-06-20

Aerodynamic and overall parameters analysis of buoyancy-lifting hybrid airship

School of Aeronautic Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China

摘要

摘要: 为了兼顾飞艇的气动性能和浮升特性,充分发挥二者的优势,并增强可控性,提出了一种基于NACA高升力翼型的组合嚢体式混合飞艇气动布局.采用计算流体力学(CFD)方法建立混合飞艇FLUENT计算模型,数值模拟了它在不同速度和迎角下的升阻特性、纵向静稳定性及浮升特性,并进行了总体性能评估,最后将其与常规飞艇进行了对比.结果表明:该组合嚢体飞艇布局具有较好的气动性能和效率,相同条件下提供的动升力为常规飞艇的3倍;当飞行速度大于26 m/s时,混合飞艇总升力效率开始大于常规飞艇,能够提供更好的浮升特性.此外,相同设计载荷下混合飞艇的外形尺寸更小,有利于增加有效载荷,可为低空大型混合飞艇的研发提供参考.
- 浮升一体 /
- 混合飞艇 /
- 气动性能 /
- 浮升特性 /
- 总体设计
Abstract: In order to balance the aerodynamic performance and buoyancy-lifting characteristics of airship, to make full use of their advantages and to strengthen the controllability, a hybrid airship configuration which has combined envelopes that are based on high lift NACA airfoil was proposed. With computational fluid dynamics (CFD) and FLUENT computing modeling, the lift-drag characteristics, longitudinal static stability and buoyancy-lifting property under different velocities and attack angles of the airship were simulated, furthermore, its overall performance was evaluated and lastly it was compared with conventional airship. The results show that the airship configuration with combined envelopes has good aerodynamic performance and efficiency. It can produce three times aerodynamic lift than that of conventional airship under the same condition. When the magnitude of cruise velocity is greater than 26 m/s, hybrid airship begins to have a higher total lift efficiency and better buoyancy-lift property. Besides, the hybrid airship's size is smaller than conventional airship under the same design load, which contributes to increasing payloads. This can provide a reference for low-attitude large hybrid airship's research.
- buoyancy-lifting /
- hybrid airship /
- aerodynamic performance /
- buoyancy-lifting characteristics /
- overall design

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参考文献(18)

[1]	Barnard L, Navid L Q, Walter T G.A new concept of hybrid airship, AIAA-1985-0868[R].Reston:AIAA, 1985.
[2]	Robert R.Performance of hybrid air vehicles[C]//Proceeding of the 40th AIAA Aerospace Sciences Meeting and Exhibit.Reston:AIAA, 2002.
[3]	Liu T S, William W L.Aeroship:A new flight platform[C]// Proceedings of the 24th AIAA Applied Aerodynamics Conference.Reston:AIAA, 2006:2652-2684.
[4]	Jeremy A, Thomas G, Fabrice K, et al.Conceptual design of a hybrid lift airship for intra-regional flexible access transport[C]//Proceedings of 48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition.Reston:AIAA, 2010.
[5]	Richard J.Operating considerations for large hybrid air vehicles[C]//Proceedings of AIAA 4th Aviation Technology, Integration and Operations(ATIO)Forum.Reston:AIAA, 2004:742-748.
[6]	李峰, 叶正寅.一种新型浮生一体化排式飞翼气动布局的设计与研究[J].力学学报, 2009, 41(6):850-857. Li F, Ye Z Y.Design and research for a new type buoyancy-lifting row flying-wings[J].Chinese Journal of Theoretical Applied Mechanics, 2009, 41(6):850-857(in Chinese).
[7]	Grant E C, Leland M N.Fundamentals of aircraft and airship design, Volume II-Airship design and case studies[M].Reston:AIAA, 2013:345-379.
[8]	Jeremy A, Thomas G, Fabrice K, et al.Conceptual design of a hybrid lift airship for intra-regional flexible access transport[C]//Proceedings of 48th AIAA Aerospace Sciences Meeting Including the New Horizen Forum and Aerospace Exposition.Reston:AIAA, 2010.
[9]	Dornheim M A.Lockheed Martin's secretly built airship makes first flight[EB/OL].America:Aviation Week and Space Technology, 2009[2014-05-12].http://www.aviationweek.com.
[10]	Carichner G E, Nicolai L M.Hybrids…the airship messiah [C]//Proceedings of 20th AIAA Lighter-Than-Air Systems Technology(LTA)Conference.Reston:AIAA, 2013.
[11]	李峰, 叶正寅, 高超.新型浮生一体化飞艇的总体性能和应用研究[J].工程力学, 2013, 30(3):437-458. Li F, Ye Z Y, Gao C.Overall performance and application research on a new type buoyancy-lifting airship[J].Engineering Mechanics, 2013, 30(3):437-458(in Chinese).
[12]	马东立, 叶川.升力浮力复合型飞艇动导数分析[J].航空动力学报, 2013, 28(5):1074-1080. Ma D L, Ye C.Dynamic derivative analysis for hybrid airship incorporating lift and buoyancy[J].Journal of Aerospace Power, 2013, 28(5):1074-1080(in Chinese).
[13]	龙飞, 黄龙太, 姜琬.某常规飞艇与混合式飞艇总体设计和性能分析[J].航空工程进展, 2012, 3(2):150-155. Long F, Huang L T, Jiang W.The overall design and performance analysis of a conventional and hybrid airship[J].Aerospace Engineering Process, 2012, 3(2):150-155(in Chinese).
[14]	张科施, 宋笔峰, 安伟刚.大载重浮升式运输飞机研究进展[C]//2007年中国浮空器大会论文集.北京:航空工业出版社, 2007:22-27. Zhang K S, Song B F, An W G.Advances in heavy-lift hybrid airship[C]//Proceedings of 2007 China aerostat conference.Beijing:Aviation Industy Press, 2007:22-27(in Chinese).
[15]	Andan A D, Asrar W, Omar A A.Investigation of aerodynamic parameters of a hybrid airship[J].Journal of Aircraft, 2012, 49(2):658-661.
[16]	GAMBIT user's guide[EB/OL].New York:Fluent Inc., 2003[2012-05-06].http://www.docin.com/p-396777275.html.
[17]	张丹, 郭雪岩.平流层双轴球体飞艇绕流场的数值分析[J].力学季刊, 2008, 29(4):556-564. Zhang D, Guo X Y.Numerical analyses on ambient flow of a double-axis ellipsoidal stratospheric airship[J].Chinese Quarterly of Mechanics, 2008, 29(4):556-564.
[18]	Nicolai L M, Carichner G E.Airplanes and airship evolutionary cousins, AIAA-2012-1178[R].Reston:AIAA, 2012.