q22 - temperature rise and the work added to the flow...

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Chapter 8, Question 2: Turbojet Performance Reproduced with the kind permission of Rolls-Royce plc. Copyright Rolls-Royce plc. Used with permission.
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Chapter 8, Question 2 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. This is produced by two effects: the ram
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Unformatted text preview: temperature rise and the work added to the flow across the compressor. Therefore the thermal efficiency is influenced both by flight Mach number (sets the increase in stagnation temperature due to the ram effect) and compressor temperature rise. Class performance (2003): 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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q22 - temperature rise and the work added to the flow...

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