ENTREE D'AIR SUPERSONIQUE BIDIMENSIONNELLE ET ASYMETRIQUE POUR L'AIR DE COMBUSTION D'UN MOTEUR D'AERONEF

摘要

The bidimensional supersonic air intake for the combustion air of an aircraft engine comprises on the one hand a front flap (3) forming a visor and on the other hand a hull (4). The front flap (3) is movable about a pivot axis (5) situated opposite the hull (4). The front flap (3) is integral with a movable hull mouth (6) situated at the front of the hull (4) and moving in front of the latter when the front flap (3) moves in the direction which increases the cross-section of the air intake. ……