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Altitude-wind-tunnel investigation of operational characteristics of J47 turbojet engine
Report presenting an investigation in the altitude wind tunnel to determine the operational characteristics of a J47 turbojet engine over a wide range of simulated flight conditions at a range of altitudes. Operational characteristics investigated include operating range, starting, altitude and airspeed compensation of the fuel regulator, and acceleration.
Date:
August 3, 1950
Creator:
Bloomer, Harry E.
System:
The UNT Digital Library