Volume 41 Issue 11
Nov.  2015
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LYU Zhenjun, WANG Jiangfeng. Design and comparative analysis of multistage compression cone-derived waverider and osculating cone waverider[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2103-2109. doi: 10.13700/j.bh.1001-5965.2014.0740(in Chinese)
Citation: LYU Zhenjun, WANG Jiangfeng. Design and comparative analysis of multistage compression cone-derived waverider and osculating cone waverider[J]. Journal of Beijing University of Aeronautics and Astronautics, 2015, 41(11): 2103-2109. doi: 10.13700/j.bh.1001-5965.2014.0740(in Chinese)

Design and comparative analysis of multistage compression cone-derived waverider and osculating cone waverider

doi: 10.13700/j.bh.1001-5965.2014.0740
  • Received Date: 27 Nov 2014
  • Rev Recd Date: 04 Jan 2015
  • Publish Date: 20 Nov 2015
  • As a forebody of hypersonic vehicle which was powered by air-breathing scramjet, waverider not only showed its excellent aerodynamic performance, but also played the role of pre-compression to incoming flow for hypersonic vehicle. In order to further enhance the waverider forebody's pre-compression effect, a new design method for multistage compression waverider configuration was presented, based on theory of osculating cone proposed by Sobieczky. Multistage compression cone-derived waverider and osculating cone waverider which had multiple compressive surfaces were obtained by using the design method. Aerodynamics performance of three-stage compression cone-derived waverider and osculating cone waverider were compared and analyzed in the same design condition and with the same projection curve of forbody. The research results show that the design expectation is in well agreement with the result of numerical simulation. The design method of multistage compression waverider can be used to cone-derived waverider and osculating cone waverider.

     

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