Performance Analyses of Fluidic Thrust Vector Control System Using Dual Throat Nozzle

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Flows in the rocket engine nozzles have been numerically analyzed to assess the performance of thrust vector control system of fluidic type by the direct simulation Monte Carlo method. Secondary je...

Journal

  • AIAA Journal

    AIAA Journal 60 1730-1744, 2019-08-16

    American Institute of Aeronautics and Astronautics (AIAA)

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