Direct measurements were undertaken at the Aeronautics Laboratory in Turin of the aerodynamic actions on an oscillating wing. The tests conducted had as their essential object the examination of the operation of apparatus designed for this measurement. The values experimentally obtained for the aerodynamic coefficients are in good agreement with the theory of oscillatory motion of the wing of finite span and show clear deviation from the values obtained by theory of plane motion.
Comparison of theory with experiment in the phenomenon of wing flutter
01.02.1939
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Englisch
Comparison of theory with experiment in phenomenon of wing flutter
Engineering Index Backfile | 1939
|Theory of wing flexure flutter
TIBKAT | 1948
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