In addition to stability derivatives, results are added for determining theoretical rolling moment due to aileron deflection and series of influence lines is given by which loading across span may be determined for any angle of attack distribution that may occur on wing plan forms considered.
Theoretical stability and control characteristics of wings with various amounts of taper and twist
Nat Advisory Committee Aeronautics -- 24th Annual Report
1938
17 pages
Bibliography
Report
Englisch
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Engineering Index Backfile | 1948
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