The ramjet performance is calculated and compared with fixed and continuous adjustable structure intake and nozzle in this paper.
本研究对具有固定、连续可调进气道和尾喷管的冲压发动机性能进行了计算和比较。
This design created a gap between the air intake and the forward fuselage, and requires six small beams to enhance the structure for high-speed flight.
这样的设计导致了机身与进气口之间有一个间隔，为了高速飞行而在之间使用了6条小加强筋以加固结构。
The operation process of the carburetor engine and EFI engine are analyzed according to the structure features of the intake system of both engines.
从电喷发动机与化油器式发动机进气系统的结构特点出发，分析了这两类发动机的工作过程。
应用推荐