An integrated study of aerodynamics, propulsion, dynamics, structures, and performance with the purpose of a design of an aircraft that meets the desired specifications. Topics include weight estimates, sizing, configuration layout, wing geometry, propulsion estimates, and stability of motion.
Prerequisites
ME 2101 and (ME 2103 or CEE 2103)
Prerequisite Courses
Last Offered
Spring 2025, Spring 2024, Spring 2023, Spring 2022