Effect of Various Blade Modifications on Performance of a 16-Stage Axial-Flow Compressor 5 - Effect on Over-All Performance Characteristics of a 20-Percent Reduction in Solidity of the Fourteenth Through Sixteenth Stage Rotors

Author: Medeiros, Arthur A.
Year: 1952
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E52D22
Link: https://digital.library.unt.edu/ark:/67531/metadc65515/

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