![]() In order to visualize the shock on the upper side of the airfoil, I'm plotting the Ma=1 line as a contour line. Just for a brief sum up for those who care Therefor I'm using a standard airfoil and use different grids and adaptation parameters and compare them in terms in regards to pressure distribution, boundary layer resolution etc. ![]() Within this study the main goal is trying to figure out the behaviour of automatic grid adaptation algorithms included in TAU. ![]() I am currently working on a seminar for university figuring out different parts of the flow solver TAU.
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