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The calculation of lateral stability with free controlsThe discussion of the structural methods for obtaining lateral stability discloses the remarkable influence of the constant fuselage and wing proportions to the yawing moments. For the effectiveness of modifications in vertical tail surfaces and tail length, these quotas - little observed heretofore, in this connection - are decisive. This also applies to the amount of dihedral of the wing with regard to the roll stability of the complete wing already existing without angle of the dihedral.
Document ID
19930094678
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Mathias, Gotthold
Date Acquired
September 6, 2013
Publication Date
April 1, 1934
Report/Patent Number
NACA-TM-741
Accession Number
93R23598
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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