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This document discusses roll control and the rate of roll achieved in aircraft. It covers topics like ailerons, differential ailerons, spoiler ailerons, rolling moment due to aileron deflection, damping moment opposed to rolling, and calculating the rate of roll based on balancing these moments. Strip theory is used to estimate lift distributions and rolling moments caused by control surface deflections and aircraft rolling motion. Equations are presented for rolling moment coefficients from ailerons and da

Author

Revathi

Language

EN