The purpose of this tutorial is to introduce the user to good techniques for modeling flow in high speed external aerodynamic applications

Transonic flow will be modeled over a NACA 0012 airfoil for which experimental data has been published, so that a comparison can be made. The flow to be considered is compressible and turbulent .The solver used is the density based implicit solver, which gives good results for high speed compressible flows

The tutorial is carried out using FLUENT and CFD Post from within Workbench, but it could also be completed in standalone mode




Availability File
Tutorial - pdf
Mesh
Case and Data

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