Theoretical stability and control characteristics of wings with various amounts of taper and twist
Description:
From Summary: "Stability derivatives have been computed for twisted wings of different plan forms that include variations in both the wing taper and the aspect ratio. Taper ratios of 1.0, 0,50, and 0.25 are considered for each of three aspect ratios: 6, 10, and 16. The specific derivatives for which results are given are the rolling-moment and the yawing-moment derivatives with respect to (a) rolling velocity, (b) yawing velocity, and (c) angle of sideslip. These results are given in such a for…
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Date:
April 19, 1938
Creator:
Pearson, Henry A. & Jones, Robert T.
Item Type:
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Report
Partner:
UNT Libraries Government Documents Department