q21 - the ratio of flight velocity to exit velocity. the...

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Chapter 8, Question 1: Turbojet Performance
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Chapter 8, Question 1 Answer The correct answer is 2) the compressor ratio across the compressor and the flight Mach number The thermal efficiency is a function of the temperature rise from atmospheric conditions to the exit of the compressor. The propulsive efficiency is a function of
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Unformatted text preview: the ratio of flight velocity to exit velocity. the overall efficiency is the product of the two and is thus influenced both by flight Mach number (flight velocity) and compressor temperature rise. Class performance (2001):...
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This note was uploaded on 01/28/2012 for the course AERO 16.01 taught by Professor Markdrela during the Fall '05 term at MIT.

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q21 - the ratio of flight velocity to exit velocity. the...

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