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Charts for the Determination of Wing Torsional Stiffness Required for Specified Rolling Characteristics or Aileron Reversal SpeedA series of charts are presented by which the wing torsional stiffness required to meet a given standard of rolling effectiveness may be quickly determined. The charts may also be used to obtain quickly the aileron reversal speed and the variation of the loss in rolling effectiveness with airspeed. The charts apply to linearly tapered wings and elliptical wings of tubular-shell construction having various aspect ratios with aileron span and location of ailerons as variables. In the derivation of the charts, induced lift effects have been taken into account and the form of the wing-torsional-stiffness curve has been assumed.
Document ID
19930091876
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Pearson, Henry A
Aiken, William S , Jr
Date Acquired
September 6, 2013
Publication Date
January 1, 1944
Report/Patent Number
NACA-TR-799
Report Number: NACA-TR-799
Accession Number
93R21166
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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