AEM 2301 - Mechanics of Flight
Standard atmospheric properties, basic aerodynamics, generation of lift/drag. Airfoils and finite wings. Elements of aircraft performance and atmospheric flight mechanics. Introduction to MatLab and simulations for aircraft design.
Prerequisites: CSE student, concurrent MATH 2373 or equiv., PHYS 1301W.
Textbook: Required: Steady Aircraft Flight and Performance, Author: N. Harris McClamroch, 2011, ISBN: 9780691147192