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Investigation of an Axial-Flow-Compressor Rotor With Circular-Arc Blades Operating Up to a Rotor-Inlet Relative Mach Number of 1.22
Author:
Robbins, William H.
Year:
1953
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E53D24
Link:
https://digital.library.unt.edu/ark:/67531/metadc59554/
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