Performance of a supersonic mixed-flow rotor with a swept leading edge and 0.52 inlet radius ratio

Author: Goldstein, Arthur W.
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E53H27
Link: https://digital.library.unt.edu/ark:/67531/metadc60020/

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