A Technique Applicable to the Aerodynamic Design of Inducer-Type Multistage Axial-Flow Compressors

Author: Savage, Melvyn
Year: 1952
Document Type: N/A
Series: NACA Technical Notes
Report Number: NACA-TN-2598
Link: https://digital.library.unt.edu/ark:/67531/metadc56242/

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