design a wing

Cerrado Publicado hace 7 años Pagado a la entrega
Cerrado Pagado a la entrega

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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Ingeniería aeroespacial Ingeniería Mathlab y Mathematica Ingeniería mecánica

Nº del proyecto: #12151450

Sobre el proyecto

9 propuestas Proyecto remoto Activo hace 7 años

9 freelancers están ofertando un promedio de $186 por este trabajo

TellezMiotta

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: Más

$250 USD en 5 días
(41 comentarios)
5.6
bchandra1955

Professional aerospace engineer can take care ..........................................................................................

$100 USD en 1 día
(121 comentarios)
6.4
Mostafahasan

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

$144 USD en 5 días
(46 comentarios)
5.2
yadavom1990

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 Más

$111 USD en 3 días
(41 comentarios)
5.3
NikoKoutsorizof

A proposal has not yet been provided

$166 USD en 1 día
(1 comentario)
2.5
diderdid

some experience to work on this kind of project shoudl be able to make me to finish on time and well.

$277 USD en 1 día
(0 comentarios)
0.0
zikist1

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 Más

$100 USD en 10 días
(0 comentarios)
0.0