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Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor 3 - Effect on Over-All Performance Characteristics on Increasing Stator-Blade Angles in Inlet Stages
Author:
Medeiros, Arthur A.
Year:
1952
Document Type:
N/A
Series:
NACA Research Memorandums
Report Number:
NACA-RM-E52B15
Link:
https://digital.library.unt.edu/ark:/67531/metadc65396/
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