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Airfoil - Inverse Design/ Shape Optimization

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Old   June 14, 2021, 04:04
Default Airfoil - Inverse Design/ Shape Optimization
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Good day,

I have a question about the following task:
Based on a given NACA profile and the pressure distribution evident from an initial simulation, I would like to generate a new profile with the same/ a very similar pressure distribution after adjusting the flow conditions.

Now I need a hint how to realize the project in ANSYS.

I have already parameterized the pressure side of the single profile in the DesignXplorer (x,y-coordinates). However, I currently do not know how I can integrate the static pressures along the PS as target values. Is for the above mentioned problem another methodology possibly more advantageous (e.g. Adjoint Solver, BladeModeler)?
Especially with respect to the later following, intended geomteric study and airfoil generation in a cascade flow.

I would be pleased about your assistance.

With kind regards
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