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Formulas for propellers in yaw and charts of the side-force derivativeGeneral formulas are given for propellers for the rate of change of side-force coefficient with angle of yaw and for the rate of change of pitching-moment coefficient with angle of yaw. Charts of the side-force derivative are given for two propellers of different plan form. The charts cover solidities of two to six blades and single and dual rotation. The blade angle ranges from 15 degrees or 20 degrees to 60 degrees.
Document ID
19930091896
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ribner, Herbert S
Date Acquired
September 6, 2013
Publication Date
January 1, 1945
Report/Patent Number
NACA-TR-819
Report Number: NACA-TR-819
Accession Number
93R21186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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