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Note on the Effects of First-Order Aerodynamic Loads on Propeller Shaft Loads with Emphasis on Counterrotating PropellersAn investigation of the 1XP excitation of inclined single-rotation propellers has indicated a new concept for determining propeller shaft forces and moments of an inclined propeller. This report presents preliminary results, in particular to the counterrotating propeller.
Document ID
20040012865
Acquisition Source
Langley Research Center
Document Type
Other - NACA Research Memorandum
Authors
Rogallo, Vernon L. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
McCloud, John L., III (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Yaggy, Paul F. (National Advisory Committee for Aeronautics. Ames Aeronautical Lab. Moffett Field, CA, United States)
Date Acquired
August 21, 2013
Publication Date
January 1, 1954
Subject Category
Aircraft Design, Testing And Performance
Report/Patent Number
NACA-RM-A54C30
Report Number: NACA-RM-A54C30
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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