Introduction To Aerodynamics

Catalog description

This course is an introductory upper-level class on aerodynamics and will cover the fundamentals of aerodynamics on fixed, rotatory and flapping wings. Classic aerodynamic theories and models, including Kutta-Joukowski theorem, lifting line theory, blade element method, disk momentum theory, quasi-steady model and etc will be explained and discussed in the class. Additionally, lab sections will be added to the class for an in-depth understanding about the subject. Permission of instructor required. Prerequisite(s): ME 31200 FOR LEVEL UG WITH MIN. GRADE OF C OR ME 31200 FOR LEVEL GR WITH MIN. GRADE OF C Course Learning Outcomes 1. Able to understand the basic concepts and theories in fixed-wing aerodynamics. 2. Able to use computer programs to solve 2D inviscid flow problem. 3. Able to use lifting line theory/vortex panel method to analysis the finite wing. 4. Able to program flow solver using blade-element momentum theory. 5. Able to use quasi-static method to analyze the aerodynamics of flapping wing. 6. Able to operate advanced flow diagnostic tools and software to study the flow of airfoil, rotatory and flapping wings. View Class Schedule