Creating Airfoil Geometry with Panel Method
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Hello everyone.
Im currently a mech. eng. student who is trying to learn. I have a project but Im stuck. Its about airfoil optimization.
Our professor gave us initial guesses and cp target values. In our code, we need to create an airfoil geo, get y values, calculate cp, find the difference between cp target and repeat. We have an example code that gives coordinates of NACA airfoils with panel method. I did the panel code for circle with no problem. My problem is about creating an airfoil geo. On the project assignment, it is written that we need to create "our own airfoil geometry". This is my problem. There is only one circle shape but possibilities for airfoil geo are unlimited. I dont know how to create one. Every example I could find on airfoil geo. with panel method used airfoil tools and/or spesific airfoil.
I would be glad if you can help me. Thanks
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