Design wing
$10-30 USD
Płatność przy odbiorze
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.
Numer ID Projektu: #12259738
O projekcie
Przyznany użytkownikowi:
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 freelancerów złożyło ofertę za $71 w tym projekcie
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: Więcej
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.
I'm a experienced MATLAB programmer and Mechanical Engineer specialized in Aeronautical projects, who is really excited to get things working. Give me more details so I can provide you a detailed plan of how we're gett Więcej