Performance of Compressor of XJ-41-V Turbojet Engine, 3, Compressor Static-Pressure Rise at Equivalent Compressor Speeds of 5000, 7000, 8000, and 9000 rpm

Author: Creagh, John W. R.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E7G03a
Link: https://digital.library.unt.edu/ark:/67531/metadc65010/

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