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Forum: OpenFOAM Running, Solving & CFD

May 28, 2013, 04:55

Replies: 17

RAE2822 transonic aerofoil

Views: 8,301

Posted By skeptik

NACA 23012 results, transonic flow

What i've got about my airfoil (exp and Fluent data were extracted from article (http://www.mai.ru/science/trudy/published.php?ID=30874), but it's in russian. originally exp data from TZAGI report)
...

Forum: OpenFOAM Running, Solving & CFD

May 28, 2013, 03:35

Replies: 17

RAE2822 transonic aerofoil

Views: 8,301

Posted By skeptik

I mean endTime of your simulation, not timeStep. ...

I mean endTime of your simulation, not timeStep.

If you have domain size about 15 m, and U approx 240 m/s, you need endTime approx 0.06. But i think it would be better to set 0.12 or higher just...

Forum: OpenFOAM Running, Solving & CFD

May 27, 2013, 08:40

Replies: 17

RAE2822 transonic aerofoil

Views: 8,301

Posted By skeptik

interesting

Hi.

I wait for your further simulations. I do airfoil at M>>0.3 too but it's NACA 23012 and i really interesting about your results.

But i have several questions about your case cause i didn't...

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