Volume 22 Issue 12
Dec.  2007
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Article Navigation >  Journal of Aerospace Power  > 2007  >  22(12): 2113-2118
HU Jian-xin, XIA Zhi-xun, ZHAO Jian-min, GUO Jian, ZHANG Wei, LUO Zheng-bing, Miao Wan-bo. Design optimization of secondary chamber response surface of boron-based propellant ducted rocket motor[J]. Journal of Aerospace Power, 2007, 22(12): 2113-2118.
Citation: HU Jian-xin, XIA Zhi-xun, ZHAO Jian-min, GUO Jian, ZHANG Wei, LUO Zheng-bing, Miao Wan-bo. Design optimization of secondary chamber response surface of boron-based propellant ducted rocket motor[J]. Journal of Aerospace Power, 2007, 22(12): 2113-2118.
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Design optimization of secondary chamber response surface of boron-based propellant ducted rocket motor

  • College of Aerospace and Material Engineering, National University of Defense Technology, Changsha 410073, China

  • Received Date: 2006-11-21
  • Rev Recd Date: 2007-04-18
  • Publish Date: 2007-12-28
    Abstract
  • There are a variety of influential factors to the combustion efficiency of secondary chamber of boron-based propellant ducted rocket motor,which are difficult to be expressed accurately by analytical functions.Atwo-phase turbulent flow combustion value simulation model was firstly established within the secondary chamber of the rocket motor.Then,the structural optimization of secondary chamber of Boron-based propellant ducted rocket motor was achieved through the response surface based on orthogonal polynomial.This method allows to compute less frequently the flow field of secondary chamber in obtaining the approximate functions,and makes it easier to optimize and analyze the parameters of secondary chamber of boron-based propellant ducted rocket motor.

     

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