
High-Speed Aerodynamics
Faculty of EngineeringDepartment of Mechanical Engineering
Description
Equations of compressible flows. Planar and conical shock waves. Expansion and shock wave interference; shock tubes. Method of characteristics. Supersonic nozzle design. Aerofoil theory in high subsonic, supersonic and hypersonic flows. Conical flows. Yawed, delta and polygonal wings; rolling and pitching rotations. Wing-body systems. Elements of transonic flows.
Course outline
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MECH537 has possible credit equivalents including ME5306 at National University of Singapore.