“Think of an airplane as a great body with its end structures (wings, horizontal tail
surfaces, vertical tail surfaces) that could have the possibility to change their shape as
they had internal nerve endings and muscles ...”
Results of the Fluid Structure Interaction analysis:
comparison between the piezo-wing and the aileron-wing
Comparison of Cl-Cd drag polar
curves for the examined wings
(h = 0 m, M = 0.17)
Comparison of Delta Mx - Non dimensional
parameter curves for the examined wings
(h = 0 m, M = 0.17 )
Comparison of Cl-Cd drag polar curves for
the examined wings
( h = 12000 m, M = 0.65 )
Comparison of Delta Mx - Non dimensional
parameter curves for the examined wings
( h = 12000 m, M = 0.65 )
