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Aeronautics 420


 
Module code MLV 420
Qualification Undergraduate
Faculty Faculty of Engineering, Built Environment and Information Technology
Module content

Introduction to aerodynamics and aeronautics. Fundamental physical quantities of flowing gas. Equations of state. Anatomy of an airplane. Atmospheriology. Basic aerodynamics. 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. Propeller theory. Elements of airplane and flight performance. Range, endurance and payload. Principles of static stability and control.

Module credits 16.00
Prerequisites MTV 310
Contact time 1 practical per week, 3 lectures per week
Language of tuition English
Academic organisation Mechanical and Aeronautical En
Period of presentation Semester 2

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