Effect of Inlet-Guide-Vane Angle on Performance Characteristics of a 13-Stage Axial-Flow Compressor in a Turbojet Engine

Author: Medeiros, Arthur A.
Year: 1956
Document Type: N/A
Series: NACA Research Memorandums
Report Number: NACA-RM-E55K23
Link: https://digital.library.unt.edu/ark:/67531/metadc62428/

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