Over-all performance of the J71 three-stage turbine
Description:
Report presenting an investigation to determine the overall performance of the three-stage turbine from the J71 turbojet engine. The turbine operated with a maximum brake internal efficiency of approximately 0.84 at an equivalent overall pressure ratio of approximately 3.6 and an equivalent rotor speed of about 110 percent of the equivalent design value.
Date:
July 9, 1952
Creator:
Berkey, William E.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department