"We are aiming for miniature systems, with low energy consumption and low cost, which may be easily integrated into structures, for example an airport room, a pipeline, a concrete slab or an aircraftwing", explains Brigitte Attal Trétout. "If we achieve this, it will be an important breakthrough
Thus, when the wake noise of an aircraftwing is to be studied, the air movements must be modeled in accordance with the profile of the wing. The direct calculations relate solely to the area downstream of the trailing edge, whereas the area upstream is assessed using statistical methods
