How to extrapolate airfoil trailing edge to make it closed?
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?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? 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? matlab, extrapolation, data MATLAB Answers — New Questions