Onera M6 wing CFD validation | Ansys Fluent | Part 1/3 (Domain Modelling)

In this tutorial video, CFD analysis and validation of Onera M6 Transonic wing using Ansys Fluent is demonstrated.
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Version: 19.3
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[@udakahewage3413]

What's the root chord of your wing?

[@LearnCAE]

Actual root chord is 805.9mm. For analysis model is scaled down with a root chord of 205.4mm

[@udakahewage3413]

@@LearnCAE Thanks