Investigation of an impulse axial-flow compressor rotor over a range of blade angles

Author: Schulze, Wallace M.
Additional Authors: Westphal, Willard R., Erwin, John R.
Year: 1950
Document Type: NACA
Issuing Agency: National Advisory Committee for Aeronautics,
SUDOC: Y 3.N21/5:15/L50F27a
Series: NACA research memorandum ;
Report Number: L50F27a
Subject: Axial flow compressors--Blades--Testing
Link: https://hdl.handle.net/2027/mdp.39015086464677

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