Performance characteristics of an axial-flow transonic compressor operating up to tip relative inlet Mach number of 1.34

Author: Creagh, John W R
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E56D27
Link: https://digital.library.unt.edu/ark:/67531/metadc62711/

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