Highly efficient transonic laminar flow wing

摘要

Improved supersonic laminar flow wing structure, on a supersonic aircraft, having strake extending forwardly of the wing inboard extent, and reversed fillet at strake junction with the wing leading edge.

主权项

1. Improved high speed laminar flow wing structure, on an aircraft, having in combination the following:
a) strake extending forwardly of the wing inboard extent, b) reversed fillet at strake junction with the wing leading edge, c) plain flap and hybrid plain-split flap structures and flap deflecting actuators therefor carried at the wing trailing edge, rearward of the strake and reversed fillet, said actuators having a pivoting axis that is collinear with a pivoting axis of said split flap.