Volume 26 Issue 4
Apr.  2011
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LI Jian-ping, SONG Wen-yan, XIAO Yin-li. Research on the optimization design of integrated scramjet /airframe[J]. Journal of Aerospace Power, 2011, 26(4): 874-879.
Citation: LI Jian-ping, SONG Wen-yan, XIAO Yin-li. Research on the optimization design of integrated scramjet /airframe[J]. Journal of Aerospace Power, 2011, 26(4): 874-879.

Research on the optimization design of integrated scramjet /airframe

  • Received Date: 2010-03-25
  • Rev Recd Date: 2010-09-27
  • Publish Date: 2011-04-28
  • A performance calculation program and an optimization design platform of integrated scramjet/airframe,including three main parts:forebody/inlet,combustor and nozzle/afterbody,were developed in this paper.The hydrogen-fueled,integrated scramjet/airframe configuration optimization design was performed based on the optimization design platform.The integrated scramjet/airframe two-dimensional configuration of optimized design was numerically simulated.The calculation results indicate that the performance calculation program of integrated scramjet/airframe is exact and the optimized design result is reliable.

     

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