Aeronautics 420

Modulekode MLV 420
Kwalifikasie Undergraduate
Fakulteit Faculty of Engineering, Built Environment and Information Technology

Introduction to aerodynamics and aeronautics. Fundamental physical quantities of flowing gas. Equations of state. Anatomy of an airplane. Atmospheriology. Basic aerodynamics. Potential flow. Elementary compressible flow. The Kutta-Joukowski Theorem. Introduction to viscous flow. Laminar and Turbulent Boundary Layers. Skin friction. Transition Flow Separation. Airfoil nomenclature. Lift, drag and moment coefficients. Pressure coefficients. Airfoil data. Wing properties. Circulation, downwash, and induced drag. Span efficiency. Stall. High-lift devices. Drag. Elements of airplane and flight performance. Range, endurance and payload. Principles of static stability and control. 

Modulekrediete 16.00
Prerequisites MTV 310
Contact time 1 practical per week, 3 lectures per week
Language of tuition Module is presented in English
Department Mechanical and Aeronautical Engineering
Period of presentation Semester 2

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