Efficient fluid dynamic and structural design and integration method to achieve extended hybrid laminar flow control

摘要

Systems and methods for secondary suctioning for an aerodynamic body are presented. A primary surface (308) is configured along a leading edge of an aerodynamic body (302), and at least one secondary suction device (314) comprising an elongated shape is configured at least a first distance from the primary surface (308). A non-suction surface is configured between the primary surface (308) and the at least one secondary suction device (314).