Performance of Compressor of XJ-41-V Turbojet Engine 2 - Static-Pressure Ratios and Limitation of Maximum Flow at Equivalent Compressor Speed of 8000 RPM

Author: Dildine, Dean M.
Year: 1947
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E7E05
Link: https://digital.library.unt.edu/ark:/67531/metadc65002/

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