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Altitude-Wind-Tunnel Investigation of Performance of Several Propellers on YP-47M Airplane at High Blade Loadings: Curtiss 732-1C2-0 Four-Blade Propeller - 4An altitude-wind-tunnel investigation has been made to determine the performance of a Curtiss 732-1C2-0 four-blade propeller on a YP-47M airplane at high blade loadings and engine power. Propeller characteristics were obtained for a range of power coefficients from 0.30 to 1.00 at free-stream Mach numbers of 0.40 and .50.
Document ID
20030064146
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Saari, Martin J. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Sorin, Solomon M. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
November 26, 1946
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-E6J23
Report Number: NACA-RM-E6J23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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