In my YouTube video called “Multi-Airfoil Source/Vortex Panel Method“, we added the capability to analyze multiple element (airfoil) systems, as opposed to just single airfoil systems. The derivations used in this code are the same as those in this derivation YouTube video. To see my single airfoil implementation, you can watch this video.
Below are the files needed to run the code. Note that I only have this code written in MATLAB. If you feel so inclined, you can update my Python code for the single airfoil implementation. You will need all of these files in the same directory. You will also need the “xfoil.exe” program in this directory (download it here). If you want to be able to load airfoils, you’ll also need a directory called “Airfoil_DAT_Selig” in this directory, which includes all the “.dat” files that can be downloaded from the UIUC airfoil database. The main file that you will run is called SPVP_Airfoil_N.m. All these files can also be found on my GitHub site.
To run this program without errors, you need to also download COMPUTE_IJ_SPM_N.m, COMPUTE_KL_VPM_N.m, STREAMLINE_SPM_N.m, STREAMLINE_VPM_N.m, XFOIL_N.m, and COMPUTE_CIRCULATION.m files. All files must be placed in the same directory/folder. You will also need the “xfoil.exe” program and a directory called “Airfoil_DAT_Selig” that includes all the airfoil .dat files.
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