Highly efficient supersonic laminar flow wing

Details Highly efficient supersonic laminar flow wing Highly efficient supersonic laminar flow wing

2011-05-24

2011-05-24

Dinh, Tien (Department: 3644)

Aeronautics and astronautics

Aircraft sustentation

Sustaining airfoils

C244S199400, C244S03500A, C244S130000

Reexamination Certificate

active

07946535

ABSTRACT:
An improved supersonic laminar flow wing structure, on a supersonic aircraft, having one or more of the following: a strake extending forwardly of the wing inboard extent, a raked wing tip, a reversed fillet at the strake or fuselage junction, an inboard leading edge flap extending over less than about 15% of the inboard wing panel span, and a hybrid plain-split flap having a lower surface portion deflectable downwardly relative to plain flap extent.

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patent: 6149101 (2000-11-01), Tracy
patent: 6935592 (2005-08-01), Morgenstern et al.

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