The work has not been graded but I like the output that was submitted to me. Is it possible for the same prof to do the next assignment I will be submitting? If possible, I will greatly appreciate it.
Provide an example solved of a swept and tapered wing using a single chordwise horseshoe vortice in order to find its aerodynamics characteristics: Cl against alpha and Cdi. It can be use any dimensions for the wing, it is an incompressible flow and the wing must be divided at least in 10 panels. I don´t mind the price
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