Effect of ailerons quantitatively investigated on basis of Prandtl's wing theory; angle of attack increased at one end and decreased at other; distribution of circulation expressed by Fourier series; distribution calculated for different aileron lengths; rolling moment, additional induced drag and yawing moment determined from distribution; relations when both ailerons are deflected in same direction. From Tokyo Imperial University -- Report of Aeronautical Research Inst., Dec. 1927.
Theoretical investigation of the effect of the Ailerons on the wing of an airplane
Nat. Advisory Committee Aeronautics -- Tech. Mem
1929
25 pages
4 Figs.
Book
English
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Theoretical investigation of rolling oscillations of airplane with ailerons free
Engineering Index Backfile | 1946
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