Volume 22 Issue 9
Sep.  2007
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Article Navigation >  Journal of Aerospace Power  > 2007  >  22(9): 1569-1572
WU Xiong, WANG Zhong-wei, JIAO Shao-qiu, ZHANG Wei-hua. Optimization of response surface of secondary gas injection thrust vector control[J]. Journal of Aerospace Power, 2007, 22(9): 1569-1572.
Citation: WU Xiong, WANG Zhong-wei, JIAO Shao-qiu, ZHANG Wei-hua. Optimization of response surface of secondary gas injection thrust vector control[J]. Journal of Aerospace Power, 2007, 22(9): 1569-1572.
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Optimization of response surface of secondary gas injection thrust vector control

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

  • Received Date: 2006-09-04
  • Rev Recd Date: 2006-12-06
  • Publish Date: 2007-09-28
    Abstract
  • The secondary gas injection thrust vector control system of a test engine was optimized using partial orthogonal-polynomial based response surface methodology (RSM) along with numerical simulation.The results show that such optimization method could reduce and save the calculation time of primary/secondary interference flow field for approximate functional equation,and enable you to optimize and analyze easily the parameters of secondary gas injection system.

     

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