Advanced Computational Aerodynamics
Faculty of EngineeringDepartment of Mechanical Engineering
Description
Explicit and implicit time-integration methods; 2D and 3D finite-difference and finite-volume formulations for subsonic, transonic and supersonic rotational flows. Shock-fitting versus shock-capturing methods. Solution of the Navier-Stokes equations using artificial compressibility. Spectral methods. Lagrangian formulation. Time-accurate methods for unsteady flows with oscillating boundaries.
Course outline
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MECH620 has possible credit equivalents including ME5306 at National University of Singapore.