Volume 30 Issue 05
May  2004
Turn off MathJax
Article Contents
Zhang Dongjun, Wang Yankui, Deng Xueyinget al. Design and computational study of waverider configuration with high performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(05): 429-433. (in Chinese)
Citation: Zhang Dongjun, Wang Yankui, Deng Xueyinget al. Design and computational study of waverider configuration with high performance[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(05): 429-433. (in Chinese)

Design and computational study of waverider configuration with high performance

  • Received Date: 18 Dec 2002
  • Publish Date: 31 May 2004
  • The design method and basic aerodynamic characteristics were studied for cone-derived waverider at Mach 6 and attack angle 0. Off-design performances of the designed waverider were also discussed, namely lift, drag and lift-drag-ratio changing with Mach number and attack angle. All the research works were finished by numerical simulation method. Results show that: the inverse-design method for the waverider configuration is successful based on inviscid conical shock wave. The biggest lift-drag ratio 3.36 considering viscous effects is obtained at Mach 6 when a proper base conical shock wave angle is chosen. A feasible flight control scheme is presented for the SSTO (single-stage-to-orbit) vehicle adopting this configuration. The favorable method of improving the lift-drag ratio of the figuration is brought forward.

     

  • loading
  • [1] Blankson M. Air-breathing hypersonic cruise prospects for mach 4-7 waverider . Journal of Engineering for Gas Turbines and Power, 1994,116(1):104~115 [2]Murice L,Rasmussen. Waverider configurations derived from inclined circular and elliptic cones[J].Spacecrift,1980,17(6):537~545 [3] 王 卓,钱翼稷. 乘波机外形设计[J]. 北京航空航天大学学报, 1999,25(2):180~183 Wang Zhuo, Qian Yiji. Waverider configuration design[J]. Journal of Beijing University of Aeronautics and Astronautics,1999,25(2):180~183(in Chinese) [4] 海 斯 W D ,普洛布斯坦 R F. 高超音速流理论[M]. 严宗毅,孙菽芬译. 北京:科学出版社,1979 Hayes W D, Probstein R F. Hypersonic flow theory[M]. Translated by Yan Zongyi, Sun Shufen. Beijing:Science Press, 1979(in Chinese) [5] Takeshi Miyagawa,Toshihiro Ohta,Riichi Matsuzaki.Experimental studies on several waverider configuration[J]. Aero Space Sci,1997,39(126):417~427 [6]Shi Yijan, Miles John B,Kakkattukuzhy Isaac.Computational fluid dynamics simulation of turbulent waverider flow field with sideslip [J]. Journal of Spacecraft and Rockets,1997,34(1):77~82
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(3939) PDF downloads(1126) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return