IMEC 4224 COMPRESSIBLE FLUID FLOW

At the end of the course, the student should be able to:

 

  • Understand how motion of gases changes thermodynamic properties
  • Determine flow properties upstream and downstream of normal shock waves
  • Calculate lift and drag on a supersonic airfoil
  • Determine flow properties in a shock tube
  • Understand how nozzles work and determine supersonic flow properties
  • Calculate changes in fluid properties for flows with friction and heat addition
Understand the basics of hypersonic and high temperature flows

Créditos

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