Investigation of a high-pressure-ratio eight-stage axial-flow research compressor with two transonic inlet stages I : aerodynamic design

Author: Voit, Charles H
Year: 1953
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E53I24
Link: https://digital.library.unt.edu/ark:/67531/metadc59882/

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