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Question
1. Features of geared turbo-fan and multi-spool compressors.
2. How is the flow for jet when P exit is less than the P ambient.
3. How is the flow for jet when P exit is grater than the P ambient.
4. How is the flow when P exit is equal to P ambient
5. Explain the P and P ambient when the throat Mach number is equal to 1 ?
6. Explain the TS diagram when lower the ambient pressure little bit more ?
7. explain in TS diagram when the ambient pressure is lower than the stagnation pressure.
8. How a flow through convergent and divergent nozzle is established ?