The flux vector splitting method is adopted to solve the 2-D Euler equations and a numerical simulation is conducted for the division-flow inlet of Dual Combustor Ramjet ( DCR) as well as the cold-mixing flow field of both flows from a dump combustor and from a supersonic inlet.

  • 采用矢通量分裂法求解2D-Euler方程组,对亚燃/超燃双重燃烧冲压发动机(DCR)进气分流流场及其双重燃烧的冷态掺混流场进行了数值模拟。

  • 互联网摘选 2025-02-21 15:31:37

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