How is the flow for jet when P exit is less than the P ambient.

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John Doe  

Dr. Doe works in the area of combustion dynamics in rocket engines. His work involves physical and numerical experiments on turbulent reacting flows in confined chambers with characteristic acoustic dimensions....

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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 ?

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Turbojet Engine Test

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Jet Engines

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