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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