design a wing
$10-30 USD
Teslim sırasında ödenir
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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Proje NO: #12151450
Proje hakkında
Bu iş için 9 freelancer ortalamada $186 teklif veriyor
Hi! My name is Fernando Téllez. I am a senior year student of electrical engineering at Universidad Simón Bolívar (USB), one of the most prestigious universities in my country (Ranked 34° at the QS University Rankings: Daha Fazla
Professional aerospace engineer can take care ..........................................................................................
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
Hi, The total estimated cost that I have mentioned is not final cost. First let's discuss about your project then we can finalize the cost. My Educational Background: Pursuing Ph.D. in Solid Mechanics in Mechani Daha Fazla
some experience to work on this kind of project shoudl be able to make me to finish on time and well.
Hi! I am an aerospace engineer, and have vast experience in matlab. i can do it. there are many methods/solvers to predict lift& drag of a wing or an airfoil e.g. VLM, Euler equations, navier-stokes etc.. and it tot Daha Fazla
