超音速冲压式喷气发动机
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。
the sh-5 was originally scheduled to carrying the yj-1 (c-101) supersonic ramjet-powered anti-ship missile for surface strike role.
5本来预定为水面打击角色携带YJ-1(C-101)超音速冲压发动机反舰导弹。
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