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Preliminary Results of an Altitude-Wind-Tunnel Investigation of an Axial-Flow Gas Turbine-Propeller Engine: Windmilling Characteristics - 2Wind tunnel investigations were performed to determine the performance properties of an axial-flow gas turbine-propeller engine II. Windmilling characteristics were determined for a range of altitudes from 5000 to 35,000 feet, true airspeeds from 100 to 273 miles per hour, and propeller blade angles from 4 degrees to 46 degrees.
Document ID
20030064121
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Conrad, E. W. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Durham, J. D. (National Advisory Committee for Aeronautics. Lewis Flight Propulsion Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
August 3, 1948
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NACA-RM-E8F10a
Report Number: NACA-RM-E8F10a
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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