Normal modes and manoeuvre analysis in a closed form aircraft dynamic model
Auditorium (AE 005), Department of Aerospace EngineeringIn this seminar, I will first introduce an empirical four-parameter formula for lift and drag on an airfoil, which shows good fits to experimental data. I will then use this formula to obtain a closed form nonlinear dynamical model of the longitudinal or pitch plane motions of an aircraft. The method of time scale separation […]