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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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