ME 5206
:
Aircraft Design
An integrated study of aerodynamics, propulsion, dynamics and control, structures, aeroelasticity, and performance with the purpose of a design of an aircraft that meets the desired specifications. Topics include weight estimates, sizing, configuration layout, airfoil and wing geometry, propulsion estimates, structual analysis, and stability of motion.
Prerequisites
ME 2101 and (ME 2103 or CEE 2103) and ME 3600