Recent content by Sonik_87

Well the formula would be: Cp = 1 - (V/U)^2 - (2/U^2)*dPHI/dt but I do not know exactly how to calculate my potential PHI from my Gammas. Do you have any idea? I have tried in a few ways but the results are not correct.

Hi everyone, I am working on a project for the development of a 2D Unsteady Panel Method for Airfoils. As often already suggested in this forum I have been using the book "Low Speed Aerodynamics" which has helped me a lot to produce the Steady State solver (I am writing the code in Matlab at...