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◦
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
Hello, dear. I am an expert in Matlab, Mathematics, Physics.... I have my a lot of experiences in many engineering tasks. I can help you well. Please contact me. Best regards.