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NASA NTRS · 19930083667

Graphical solution of some automatic-control problems involving saturation effects with application to yaw dampers for aircraft

Phillips, William H
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STABILITY, LATERAL AND DIRECTIONAL - DYNAMICCONTROL, AUTOMATICSTABILIZATION, AUTOMATIC

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Phillips, William H. 1953-10-01. Graphical solution of some automatic-control problems involving saturation effects with application to yaw dampers for aircraft. https://ntrs.nasa.gov/citations/19930083667

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NASA NTRS1956

Calculation of the forces and moments on a slender fuselage and vertical fin penetrating lateral gusts

A theory is presented for calculating the variation with frequency of the lateral-force and yawing-moment coefficients due to sinusoidal side gusts passing over the profile of a simple fuselage-vertical-fin combination. The analysis is based on slender-body theory. The method considers the penetration effect of both fuselage and vertical tail in calculating side force and yawing moment due to side gusts, as opposed to a simple lag concept which considers the flow angle to be uniform over the configuration.

STABILITY, LATERAL AND DIRECTIONAL - DYNAMIC↗