3.00 Credits
This course is an analysis of the physics of flight. The course includes application of basic aerodynamics to the wing and airfoil, analysis of lift and drag components relative to the wing platform and airplane performance, and application of aerodynamic effects of turbojet engines involving principles of propulsion. 3-0-3 Co-Requisite: MATH 126, MATH 129, MATH 130, MATH 155, or MATH 160