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MECH 539 Computational Aerodynamics (3 credits)

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Offered by: Mechanical Engineering (Faculty of Engineering)

Overview

Mechanical Engineering : Fundamental equations. Basic flow singularities. Boundary element methods. Source, doublet and vortex panel methods for 2D and 3D incompressible and compressible flows. Method of characteristics. Euler equations for inviscid rotational flows. Finite-difference and finite-volume methods. Explicit and implicit time-integration methods. Quasi 1D solutions. Nozzle and confined aerofoil applications.

Terms: This course is not scheduled for the 2010-2011 academic year.

Instructors: There are no professors associated with this course for the 2010-2011 academic year.

  • (3-0-6)
  • Prerequisite: MECH 309 or MATH 317, MECH 533.
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