Develop a numerical method using any programming language (i.e., Matlab, Fortran, C, etc.) to predict the performance of a wing. Use the code to design a trapezoidal wing by stating the airfoil selection, aspect ratio, taper ratio, and aerodynamic twist. Predict the lift coefficient, lift distribution, circulation distribution, and induced dragcoefficients for different angles of attack,α = 0◦, 2◦, 4◦, 6◦, and 8◦
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Hi , I am an aerospace engineer with perfect experience in Aerodynamics and Matlab. Please if you are interested contact me to discuss more detail. Thanks and best regards, Mostafa Hasan
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