To sum up, Professor Joukowski's theory of supporting wings renders it possible to calculate the coefficient of lift in terms of the angle of attack, and Prandtl's coefficient of induced drag and the correction of the angle of attack in terms of the disposition and aspect ratio of the wings.
Joukowski wings
1922-04-01
Sonstige
Keine Angabe
Englisch
Graphic Construction of Joukowski Wings
NTRS | 1979
|Pressure Distribution on Joukowski Wings
NTRS | 1979
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