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 coecient, lift distribution, circulation distribution, and induced drag coecients for dierent angles of attack,
= 0, 2, 4, 6, and 8.
Hi , I am an aerospace engineer with perfect experience in Aerodynamics and MATLAB . I can do that project using lifting line theory. Please if you are interested contact me. Thanks and best regards, Mostafa Hasan
8 Freelancer bieten im Durchschnitt $71 für diesen Job
Hello Sir/mam I have done same project for one of my student successfully ,so I can give very good results at short period of time please open chat with me and we will discuss further
I can make a Vortex lattice method code in MATLAB for you. The only thing that it can't do is predicting stall performance and accounting for wing thickness. If that is ok, let me know and we can take it further.