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
Wonderful project! We are pro in Matlab. We are masters of Mathematics and Control Engineering. So we will finish your project in time. Keep in touch with us. Thanks a lot.
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.