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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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