Investigation of a 10-stage subsonic axial-flow research compressor V : effect of reducing inlet-guide-vane turning on over-all and inlet-stage performance

Author: Budinger, Ray E
Year: 1954
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E53H10
Link: https://digital.library.unt.edu/ark:/67531/metadc59693/

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