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Aerospace Courses on NPTEL  

Amardip Ghosh
IIT Kharagpur, India

 

 

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Question bank

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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