“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 ...”
Velocity, wingspan section @ 6 m (h = 0
m, M = 0.17, δa=5°, αg = 0°)
Cp, wingspan section @ 6 m (h = 0 m, M
= 0.17, δa=5°, αg = 0°)
Cp, wingspan section @ 6 m (h = 12000
m M = 0.65, δa=-5°, αg = 0°)
FSI analyses: deformed
shape with downward rotation
of aileron
(h = 12000 m, M = 0.65,
δa=5°, αg = 0°)
Fluid dynamic grid relevant to the aileron of the standard wing
(page 2 of 2)
