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Altitude-wind-tunnel investigation of thrust augmentation of a turbojet engine 3: performance with tail-pipe burning in standard-size tail pipe
From Introduction: "Evaluation of tail-pipe burning in this engine with a larger tail-pipe combustion chamber is discussed in reference 1. Results of investigations on tail-pipe burning in this engine at static sea-level conditions are presented in reference 2. An investigation of thrust augmentation by means of injecting water at the inlet of an axial-flow compressor engine is discussed in reference 3."
Date:
August 11, 1947
Creator:
Fleming, William A. & Golladay, Richard L.
System:
The UNT Digital Library
THE EXTRACTION OF IONIUM BY ORGANIC SOLVENTS
None
Date:
August 11, 1947
Creator:
Hyde, E.K. & Tolmach, J.
System:
The UNT Digital Library