Spanwise tailoring of divergent trailing edge wings

Details Spanwise tailoring of divergent trailing edge wings Spanwise tailoring of divergent trailing edge wings

B - Operations, Transporting

64

C

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

Patent

CA 2430107

A method for forming a transonic wing that segregates a baseline transonic wing into a plurality of airfoil segments that are collectively modified and optimized so as to tailor a spanwise variation of the baseline transonic wing in a manner that includes the optimized airfoil segments. An improved wing is also provided.

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