ME 5206 :
Aircraft Design

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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

Overview

Program

Mechanical Engineering

Credits

Credits 3

Last Offered

Spring 2024, Spring 2023, Spring 2022, Spring 2021