Performance of Axial-Flow Supersonic Compressor of the XJ55-FF-1 Turbojet Engine. IV - Analysis of Compressor Operation over a Range of Equivalent Tip Speeds from 801 to 1614 Feet Per Second

Author: Graham, Robert C.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-SE9J14
Link: https://digital.library.unt.edu/ark:/67531/metadc65233/

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