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What is Ideal Ramjet Engine Cycle Explained about?
The document discusses the ideal operation of a ramjet engine. It explains that a ramjet cannot produce thrust when stationary and requires an initial acceleration to a high speed, such as from a rocket or being dropped from a plane. It then describes the three main components of a ramjet - the intake, combustion chamber, and nozzle. The ideal thermodynamic cycle is presented, where there are no pressure losses and equal total temperatures and pressures at the inlet and outlet, resulting in thrust generatio
- Author
- whyfive
- Language
- EN