Component performance investigation of J71 experimental turbine 1: Over-all performance with 97-percent-design stator areas
Description:
From Summary: "The over-all component performance characteristics of a J71 experimental three-stage turbine with 97 percent design stator areas were determined over a range of speed and pressure ratio at inlet-air conditions of approximately 35 inches of mercury absolute and 700 degrees R. The turbine break internal efficiency at design operating conditions was 0.877; the maximum efficiency of 0.886 occurred at a pressure ratio of 4.0 at 120 percent of design equivalent rotor speed. In general,…
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Date:
April 11, 1956
Creator:
Schum, Harold J. & Davison, Elmer H.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department