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An improved approximate method for calculating lift distributions due to twist
Document ID
19930082939
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Sivells, James C
Date Acquired
August 16, 2013
Publication Date
January 1, 1951
Report/Patent Number
NACA-TN-2282
Accession Number
93R12229
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
LIFT DISTRIBUTION - WINGS, SWEPTBACK
THEORIES - AIRFOILS LIFTING-LINE
WINGS, TWISTED
LIFT DISTRIBUTION, WING-SPAN

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