Volume 25 Issue 2
Feb.  1999
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Wang Zhuo, Qian Yiji. Waverider Configuration Design[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(2): 180-183. (in Chinese)
Citation: Wang Zhuo, Qian Yiji. Waverider Configuration Design[J]. Journal of Beijing University of Aeronautics and Astronautics, 1999, 25(2): 180-183. (in Chinese)

Waverider Configuration Design

  • Received Date: 03 Nov 1997
  • Publish Date: 28 Feb 1999
  • The computation of generating waverider configurations using the theories of conical flow field,OC(Osculating Cone) and OA (Osculating Axisymmetric) flows are presented. Investigation shows that the method of using conical flow field theory is relatively simple and the lift-to-drag ratio of the configuration generated is high. But the inlet flow field is not quite uniform and thus it is not beneficial to the engine. The inverse design of using OA and OC theories accompanied with the inverse characteristic method can get the most universal waverider configurations and improve the inlet flow field quality and the volume efficiency effectively. Additionally, these methods have high speed of computation,which is quite promising for the integration design and optimization process later.

     

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  • 1. He X, Emanuel G. Nonslender waveriders.AIAA-93-3487-CP,1993 2. Sobieczky H. Hypersonic waverider design from given shock waves. In:Anderson J D,ed.Proceedings of the first International Hypersonic Waverider Symposium. Maryland:University of Maryland,1990 3. Sobieczky H, Zores B, Wang Z,et al. High speed flow design using osculating axisymmetric flows. In:He J J, ed. Proceedings of the third Pacific International Conference on Aerospace Science and Technology. Xi'an:Shanxi Science and Technology Publishing House, 1997. 182~187 4. 钱翼稷. 超音速轴对称有旋流特征线法的计算程序. 北京航空航天大学学报,1996, 22(4):454~459
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