How to extrapolate airfoil trailing edge to make it closed?
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Hi everyone.
I am working on airfoils right now. When l plot the data, airfoil trailing edge comes open. l tried the accepted answer on this link ( https://www.mathworks.com/matlabcentral/answers/279331-extrapolation-and-estimation-of-data ), but it didn't work for me (gives unrelated negative values). Can anyone help me to solve this problem?
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Ayush Anand
el 24 de Mayo de 2024
I can't reproduce the results without the actual data you are importing from "data.xlsx". If its not private data, would you mind sharing that as well?
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