zeeshaniqbalkhan / airfoilann Goto Github PK View Code? Open in Web Editor NEW 24.0 3.0 8.0 45.82 MB Official repository of paper, entitled "Airfoil’s Aerodynamic Coefficients Prediction using Artificial Neural Network". Home Page: https://ieeexplore.ieee.org/document/9990112 License: MIT License Python 82.02% MATLAB 17.98% aerodynamics airfoils machine-learning artificial-neural-networks Introduction · People · Discuss
how to dowload and use the code on pc how do irunn this code on mylaptop as icansee there are alotof missing modules kindly help
Supersonic training Hi, I have read your work and from the article I read that you assumed an incompressible flow (M= 0.1-0.3). In your opinion could I train the ANN for a wider range of fligh conditions?
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