The present work investigates, on the basis of Prandtl's wing theory, the form of the lift distribution when the ailerons are deflected in opposite directions. An ideal fluid and a wing with a rectangular form are assumed. The moments must not cause any rotation of the wing or any deviation from the rectilinear motion.
:Theoretical investigation of the effect of the ailerons on the wing of an airplane
1929-04-01
Sonstige
Keine Angabe
Englisch
Theoretical investigation of the effect of the Ailerons on the wing of an airplane
Engineering Index Backfile | 1929
|Theoretical investigation of rolling oscillations of airplane with ailerons free
Engineering Index Backfile | 1946
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