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A semiempirical method for estimating the rolling moment due to yawing of airplanes
Document ID
19930082704
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Campbell, John P
Goodman, Alex
Date Acquired
August 29, 2013
Publication Date
December 1, 1949
Report/Patent Number
NACA-TN-1984
Report Number: NACA-TN-1984
Accession Number
93R11994
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - NACA 65A008 LOW DRAG
SIDESLIPPING
WINGS, SWEPTBACK
STABILITY - LATERAL
AIRFOILS, BICONVEX
AIRFOILS - NACA 651012 LOW-DRAG
AIRFOILS - NACA 65(06)-006 5 LOW-DRAG
AIRFOILS - NACA 0012 WING FLAPS
WINGS, RECTANGULAR
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