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A new relation between the induced yawing moment and the rolling moment of an airfoil in straight motionIn this report, the induced yawing moment, due to the rolling moment produced by the ailerons, is computed. This induced yawing moment is the greatest part of the entire yawing moment encountered by the wings.
Document ID
19930091263
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Munk, Max M
Date Acquired
September 6, 2013
Publication Date
January 1, 1925
Report/Patent Number
NACA-TR-197
Report Number: NACA-TR-197
Accession Number
93R20553
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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