Spanwise tailoring of a trailing edge wedge to a wing

B - Operations – Transporting – 64 – C

Patent

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Details

B64C 3/28 (2006.01) B64C 3/10 (2006.01) B64C 3/14 (2006.01)

Patent

CA 2431383

A method for forming a trailing edge wedge for a wing wherein the size and configuration of a trailing edge wedge at various points along the span of the trailing edge wedge are adjusted and analyzed in an iterative manner to form an improved trailing edge wedge. An improved wing assembly is also provided.

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