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MECH 620 Advanced Computational Aerodynamics (4 credits)

Offered by: Mechanical Engineering (Faculty of Engineering)

Administered by: Graduate Studies

Overview

Mechanical Engineering : 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.

Terms: This course is not scheduled for the 2013-2014 academic year.

Instructors: There are no professors associated with this course for the 2013-2014 academic year.

  • Evening course