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School:
UC Aerospace, Civ and Mech Eng
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Campus: University College Campus
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Career: Undergraduate
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Units of Credit: 3
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Contact Hours per Week: 2
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Description
This course introduces the student to the fundamentals of aerodynamics and flight mechanics. The following topics will be treated: Basic aircraft components; Properties of liquids and gases; The International Standard Atmosphere and its descriptive elements; Altimetry and airspeed; Fluid flow - boundary layers, laminar and turbulent flow; Subsonic and supersonic flow - Shock waves and Mach Number; Bernoulli's equation and dynamic pressure; Air resistance - form drag and skin friction; Aerodynamic lift and airfoils - stagnation point, pressure coefficient, centre of pressure and pitching moments; Wing characteristics - downwash and induced drag; Introduction to propulsion, propellers, turbojets and rockets.
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