As I see it, if you're going to calculate a twin-spool turbojet engine, you
- Determine expected max aircraft speed, and engine thrust at that speed and when stationary.
- Calculate peak mass of air flow
- Calculate energy needed to propel this mass of air
- Calculate bypass ratio
- Calculate compressor properties
And from here I have no idea where to move on. Some books I've read just go through the engine from compressor to exhaust nozzle, but none explains which parameter of the engine is primary and where do calculations start and how they're performed.
Would you give me a clue? Thank you!