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Inlet Icing and Effectiveness of Hot-Gas Bleedback for Ice Protection of Turbojet Engine
Report presenting an investigation of icing and ice protection at the inlet of a turbojet engine in the altitude wind tunnel. A method of ice protection was studied that uses hot gas bled from a turbine inlet and injected into the air stream ahead of the compressor inlet. Ice was either prevented or accumulated slowly at various engine speed levels.
Date:
November 26, 1948
Creator:
Fleming, William A. & Saari, Martin J.
System:
The UNT Digital Library