Performance of 24-inch supersonic axial-flow compressor in air 2: performance of compressor rotor at equivalent tip speeds from 800 to 1765 feet per second

Author: Johnsen, Irving A.
Additional Authors: Wright, Linwood C.
Year: 1949
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E8G01
Link: https://digital.library.unt.edu/ark:/67531/metadc57672/

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