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Campus: Kensington Campus
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Career: Undergraduate
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Units of Credit: 6
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Contact Hours per Week: 6
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Enrolment Requirements:
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Prerequisite: AERO3610
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Description
One-dimensional gas flow. Thermodynamic and sonic speed relations; Mach number, isentropic variable area flow, Prandtle Meyer flow, normal and oblique shock waves. Method of characteristics. Compressible potential flow. Viscous flow; method of calculating viscous drag. Engine intakes; subsonic, supersonic, ramjets, gas turbines, piston engines, design performance. Rockets. Noise. Pollution.
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