Device for enhancing the performance of aerodynamic systems and aircraft by vibrating strings on wings and rotor blades.

摘要

The invention has for its object to increase the performance of aerodynamic systems and aircraft. This object is achieved in that are arranged in the boundary layer region of the wings and rotors strings so that they are set in motion by the air flow. If, due to the shape, the flow to oscillate is insufficient, the back pressure can be directed from the inside to the strings. The desired oscillation of the strings according to the invention produces a highly turbulent intermediate layer to the laminar flow at the boundary layers of the wings / rotors. Due to the highly turbulent interlayer, the atmospheric pressure of the laminar flow on the boundary layer is strongly influenced and buoyancy boosts.