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We've finally reached the last video in my panel method series. Here, I'll show you how to update my single-airfoil SPVP code to be able to solve multi-airfoil systems. After explaining the updates (which takes about 20 minutes), we'll go through some examples of different airfoils and systems. ===== CODE ===== ► My website http://www.joshtheengineer.com/2020/0... ► GitHub https://github.com/jte0419/Panel_Methods ===== RELEVANT VIDEOS ===== ► Panel Methods Playlist • How To: Run XFoil from MATLAB ► Source Panel Method: Airfoil • Source Panel Method: Airfoil ► Vortex Panel Method: Airfoil • Vortex Panel Method: Airfoil ► Source/Vortex Panel Method: System of Equations • Source/Vortex Panel Method: System of... ► Source/Vortex Panel Methods: Airfoil • Source/Vortex Panel Method: Airfoil ===== NOTES ===== → I haven't coded this particular script in Python, and I'm not sure if I'm going to. You can download my single-airfoil SPVP code and update it based on my MATLAB code if you want to. → More airfoils and more panels per airfoil will cause the streamline calculations to take longer. → The grid for the streamline has to have equal X and Y points at the moment. I know there's an error since it doesn't work for irregular grids, but I'm not planning on fixing it at the moment. ===== ERRORS ===== → If you see an error in the video, please let me know and I will include it here. ===== REFERENCES ===== Note: the links are Amazon affiliate links. If you do happen to want to buy the book and use the link below, it helps me out a little. ► Fundamentals of Aerodynamics, Anderson https://amzn.to/3emVuXU ► Foundations of Aerodynamics, Kuethe and Chow https://amzn.to/2yMg1Vi ► Theory of Wing Sections, Abbott and Doenhoff https://amzn.to/2wvZyUt