This course provides a graduate-level introduction to static and dynamic aeroelasticity, for conventional aircraft.Students will be presented with analytical and computational techniques used to model and simulate aeroelasticity. Topics covered will be chosen from: divergence; aileron reversal; airload redistribution; sweep effects; unsteady aerodynamics; and flutter of wings. Students cannot receive credit for this course if they have taken AE/ME 5382 “Aeroelasticity”.
Recommended Background
AE 4712 or equivalent course.