System for aerodynamic flows and associated method

Aeronautics and astronautics – Aircraft sustentation – Sustaining airfoils

Reexamination Certificate

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C244S208000

Reexamination Certificate

active

07635107

ABSTRACT:
A system and method for controlling boundary layer flow over an aircraft wing are provided. The system includes at least one wing element, and a plurality of ports defined in the wing element and in fluid communication with one another. The system also includes at least one fluidic device operable to continuously ingest the fluid through at least one of the ports and eject the fluid out of at least one other port to control boundary layer flow of the fluid over the wing element.

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PCT Notification of Transmittal of the International Search Report and the Written Opinion of The International Searching Authority, or the Declaration, mailed Feb. 9, 2007 for PCT/US2006/029134 (Filed Jul. 26, 2006).

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