An aircraft trailing edge device, coupled with an aircraft wing, provides a reduction in jet-flap interaction noise while preserving the aerodynamic load capacity of the trailing edge. Embodiments of the present invention provide a trailing edge flap device that includes a center flap portion and outer edge portions, where the center flap is shorter in length in comparison to the outer edges. Additionally, the center flap is curved in the planform of the trailing edge device.

This work was done by Michael J. Czech of The Boeing Company and Russell H. Thomas of Langley Research Center. For more information on this technology, contact Langley Research Center at This email address is being protected from spambots. You need JavaScript enabled to view it.. Refer to LAR-17831-1