| 摘要 |
<p>An aerodynamic profile is described, comprising at least one portion of aerodynamic profile (1) composed of at least one first supporting profile (3a) and at least one second supporting profile (3b) adapted to support at least one layer of coating material of such portion of aerodynamic profile (1), such portion of aerodynamic profile (1) further comprising at least first actuating means (5) adapted to cooperate with at least one of such supporting profiles (3a) or (3b) to modify IDeltaTheta [ a value of incidence |theta| of such profile with respect to the other supporting profile around at least one rotation axis (R-R) parallel with an opening (A) of such portion of aerodynamic profile (1).</p> |
