Altitude-wind-tunnel investigation of compressor performance on J47 turbojet engine (open access)

Altitude-wind-tunnel investigation of compressor performance on J47 turbojet engine

From Introduction: "The effects of variations in altitude, flight Mach number, and exhaust-nozzle-outlet area on the compressor performance characteristics are graphically presented. A complete tabulation of the compressor performance data is also presented."
Date: November 22, 1949
Creator: Prince, William R. & Jansen, Emmert T.
System: The UNT Digital Library