| 摘要 |
The present invention relates to a method for actively deforming, by feedback control, an aerodynamic profile (1) comprising an elastic material (3), applied to a part of the surface of the aerodynamic profile (1), said elastic material being in contact with a fluid flow (7); said elastic material being able to be deformed by one or more shape memory actuators (4, 22, 23, 24, 25) placed in contact with the elastic material, said actuators being controlled by a computer (5) connected to sensors (8). This method applies notably to a deformation of an aerofoil of a wing of an aircraft in flight, notably subsonic. |
