NASA NTRS · 19880000433
Yaw Control At High Angles Of Attack
Abstract
Hinged, conformal forebody strakes provide control when rudders become ineffective. Device consists of symmetric pair of longitudinally hinged strakes designed to fold completely into forebody contour. Strakes rotate individually out into external flow. Asymmetric flow produced by deployed strake generates sideward force causing aircraft to yaw.
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Murri, Daniel G., Rao, Dhanvada M.. 1988-09-01. Yaw Control At High Angles Of Attack. https://ntrs.nasa.gov/citations/19880000433
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