Hello everyone,
I have problem on settings of farfield boundary condions. I want to increase turbulence intensity on the airfoil as inlet turbulence intensity but if i enter %2 , it decreases to 0.9% on the point front 1 meter from leading edge. I want to know if there is any equation of Turbulence intensity for C shape mesh domain on airfoil to have needed turbulence intensity.
Waiting for your comments.
Thank you so much...
Respected Sir
my humble help to you:
https://eprints.soton.ac.uk/412650/1/Final_thesis_Dogan_25476246.pdf
https://www.engr.uvic.ca/~ndjilali/Papers/IJCFD_Peneau%20et%20al_2004.pdf
https://pdfs.semanticscholar.org/405a/0f0bf4faaa91670b8585bc75858b5ffffe26.pdf
https://www.hindawi.com/journals/ijae/2016/7347106/
https://web.stanford.edu/group/ctr/ResBriefs99/henningson2.pdf
With respect
you must increase the Standard deviation of wind speed by increasing the flow oscillations.
Dušan Regodić
Sir, Thank you for your reply;
I study on airfoils and generally in the literature, scientist works on experimental and it is hard to find numerical solution. My y+
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