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- W217007818 abstract "The J33-A-27 compressor was operated at an inlet pressure of 14 inches of mercury absolute and ambient inlet temperature over a range of equivalent impeller speeds from 6100 to 11,800 rpm. At the design equivalent speed of 11,800 rpm, the J33-A-27 compressor had a peak pressure ratio of 4.40 at an equivalent weight flow of 105.7 pounds per second and a peak adiabatic temperature-rise efficiency of 0.745. The maximum equivalent weight flow at design speed was 113.5 pounds per second." @default.
- W217007818 created "2016-06-24" @default.
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- W217007818 date "1949-07-11" @default.
- W217007818 modified "2023-09-24" @default.
- W217007818 title "Performance of J33-A-27 Turbojet-Engine Compressor. 1; Center for Infrastructure Engineering Studies" @default.
- W217007818 hasPublicationYear "1949" @default.
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