|May 22, 2014, 03:37||
Join Date: Apr 2014
Posts: 19Rep Power: 4
I'm trying to optimize a shape of an airfoil with adjoint method. Instead to define a new boundary condition for Ua (due to my cost-function) I've calculated the value of Ua on the airfoil-boundary manually.
But I don't really know, whether it was "legal" ?
The solution of adjoint equations doesn't converge, and that is the main problem...
Thanks in advance for every comment,
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