“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 ...”
Fluid dynamic grid relevant to the aileron of the standard wing
(page 1 of 2)
Blocking procedure (zoom view)
Volume mesh (zoom view)
Grid motion due to downward
rotation of the aileron
FSI analyses: deformed shape with
downward rotation of aileron
(h = 0 m, M = 0.17, δa=5°, αg = 0°)
