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SU2 additional input boundary field

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Old   November 17, 2016, 04:37
Default SU2 additional input boundary field
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Martin Simon
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Hello guys!

I am researching advantages of applying air jets to enhance wing/blade performance.

Similar to this: http://www.scer.rpi.edu/cefpac/wp-co...d-2_Page_4.jpg

Is there a way to produce such an analysis on SU2? (e.g create a boundary face like in OpenFOAM)

I have come across many others who have been struggling with this question, but no answers yet. :/

Thank You!
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aerodynamics, blade, su2, synthetic jet, wing

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