L19_Ideal_Turbojet

L19_Ideal_Turbojet - Turbojet Mission Parameters Mach...

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Unformatted text preview: Turbojet Mission Parameters: Mach number 0 - 0.85 > 0.85 Altitude 0-12km ~12km Ambient T Ambient a 288-217 K 340-295 m/s 217 K 295 m/s T4o = 1600 K rc = 25 Performance of an ideal turbojet engine as a function of flight Mach number. M = 0.85, and M=1.2 Altitude = 12 km T4o = 1400 K M = 0.85 Altitude = 12 km T4o = 1400 K, and T4o = 1800 K Performance of an ideal turbojet engine as a function of compressor pressure ratio and flight Mach number Performance of an ideal turbojet engine as a function of compressor pressure ratio and turbine inlet temperature ...
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This note was uploaded on 04/11/2008 for the course AEM 4203 taught by Professor Schwartzentruber during the Spring '08 term at Minnesota.

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