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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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