Altitude-wind-tunnel investigations of thrust augmentation of a turbojet engine 1: Performance with tail-pipe burning
Description:
From Introduction: "Performance results of the tail-pipe burning investigation on the TG-180 turbojet engine and a comparison of experimental results with theoretical calculations are presented."
Date:
September 25, 1946
Creator:
Fleming, W. A. & Dietz, R. O.
Item Type:
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