This preview shows pages 1–3. Sign up to view the full content.
This preview has intentionally blurred sections. Sign up to view the full version.View Full Document
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):...
View Full Document
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.
- Fall '05