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An Application of Lifting-surface Theory to the Prediction of Angle-of-attack Hinge-moment Parameters for Aspect Ratio 4.5 Wings
Document ID
19930082115
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Jones, Arthur L
Flanagan, Mildred G
Sluder, Loma
Date Acquired
August 16, 2013
Publication Date
September 1, 1947
Report/Patent Number
NACA-TN-1420
Report Number: NACA-TN-1420
Accession Number
93R11405
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AIRFOILS - ANGLE OF ATTACK
THEORIES - AIRFOILS - LIFTING-SURFACE
DOWNWASH
LOAD DISTRIBUTION, WING-SPAN
AIRFOILS - NACA 0009-0015 - LOW-DRAG (TAIL SURFACE)
AIRFOILS - ASPECT RATIO
CONTROL SURFACES - HINGE MOMENTS
AIRFOILS - NACA 65(216)-014 - LOW-DRAG (TAIL SURFACE)
LIFT DISTRIBUTION - WINGS
AIRFOILS - NACA 0012-64 (MOD ) - TAIL SURFACE

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