NACELLE DE REACTEUR POUR AVION SUPERSONIQUE

摘要

The nacelle has an air intake structure (6) including an inlet side (9) that presents a conical section defined by intersection of an elliptical shock wave generated by a conical compression ramp (16) and a plane (10). The plane is inclined with respect to another plane orthogonal to longitudinal direction of the nacelle, such that a free side of the side (9) is withdrawn in an air intake direction with respect to a side (14). An independent claim is also included for a supersonic aircraft including an engine nacelle.