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A simple method of estimating the subsonic lift and damping in roll of sweptback wings
Document ID
19930082534
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Polhamus, Edward C
Date Acquired
August 29, 2013
Publication Date
April 1, 1949
Report/Patent Number
NACA-TN-1862
Report Number: NACA-TN-1862
Accession Number
93R11824
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
THEORIES - AIRFOILS - LIFTING-LINE
WINGS, SWEPTBACK & SWEPTFORWARD - CHARACTERISTICS
WINGS - CHARACTERISTICS
AIRFOILS - NACA 0012 (APPROX )
THEORIES - FLOW - PRANDTL & GLAUERT
AUTHOR
THEORIES - AIRFOILS - LIFTING-SURFACE
ROLLING MOMENTS - WINGS
DAMPING IN ROLL
AIRFOILS - NACA 0012

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