We both were given 100 airfoils to analyze using XFOIL/XFLR5. We split the airfoils to 50 each and proceeded to extract data using these software. Inputs were fed into the XFLR5 software whereby the NACA geometries, the angles of attack and the Reynolds Numbers were entered. The outputs were manually saved and stored into a databank of more 1500 files. These will then be batch processed using MATLAB this week. Andrew will update a video of this process.
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Regression Analysis of Aerodynamic Characteristics for 87 NACA 5-Digit Airfoil Classes
Regression analysis was employed to investigate the complex relationship between the aerodynamic characteristics of NACA 5-digit airfoils an...
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A short video on PCA. Enjoy😁 Author: Andrew Clinton
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When considering all six variables, the Correlation plot that is derived appears to be inconsistent, with some variables showing minimum t...
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Welcome to this short video where we'll explore how regression analysis was employed to understand the aerodynamic characteristics of NA...
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