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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