Investigation of the effect of velocity diagram on inlet total-pressure distortions through single-stage subsonic axial-flow compressors

Author: Ashby, George C , Jr
Year: 1957
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-L57A03
Link: https://digital.library.unt.edu/ark:/67531/metadc63459/

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