Performance of an impulse-type supersonic-compressor rotor having a mean turning of 114 degrees

Author: Goldberg, Theodore J.
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L56J01
Link: https://digital.library.unt.edu/ark:/67531/metadc62862/

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