A full-automatic measuring and control system for a supersonic jetexhaust flow field is provided.
提出一套用于对超音速尾喷流流场进行全自动测试与控制的系统。
2
In a reversal of current design trends the MIT concept increases the bypass ratio by minimizing expansion of the overall diameter of the engine and shrinking the diameter of the jetexhaust instead.
与现行设计趋势相反，麻省的概念通过最小化发动机总体直径的尺度以及相应缩小喷气排放直径来增加涵道比。
3
This paper presents a no-contact temperature measurement for a small rocket engine jetexhaust, for a shock wave on nose cone of a model in a jetexhaust and for a model surface of various materials.