L19_Ideal_Turbojet

L19_Ideal_Turbojet - Turbojet Mission Parameters Mach...

Info iconThis preview shows page 1. Sign up to view the full content.

View Full Document Right Arrow Icon
This is the end of the preview. Sign up to access the rest of the document.

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 ...
View Full Document

{[ snackBarMessage ]}

Ask a homework question - tutors are online