Three Dimensional Numerical Simulation in Liquid Rocket Engine with the Method of Parallel Processing Technique
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    Abstract:

    The complex three dimensional flow field in liquid rocket engine is simulated with the method of predictive and corrective MacCormack scheme, and the parallel computation is carried out under the PVM circumstance which is made up of network of microcomputer. The results show that parallel and distributed method can play an important role on the numerical simulation in liquid rocket engine.

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History
  • Received:October 19,1998
  • Revised:
  • Adopted:
  • Online: November 18,2013
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