In this paper, using the method of numerical simulation, is studied the forming process of flow field structure in a stepped rocket launcher tube when a supersonic jet exhausts into the tube.

  • 本文以数值模拟为手段,研究了超音速燃气射流喷入阶梯型火箭发射管后,管内流场结构的发展过程。

  • 互联网摘选 2025-01-20 13:18:17

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