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March 8, 2021, 13:33
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Hypersonic Flow Simulation problem
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New Member
Ash
Join Date: Feb 2021
Posts: 20
Rep Power: 5  |
Hi,
I am currently modelling a basic re-entry flow simulation around a body, but I am not getting the results that I should be expecting, my temperature contours and velocity contours are showing no variation along the body after >15000 iterations. My initial conditions are as follows: BC: Pressure Far Field = Mach 15 No slip wall (around the body) S-A Turbulence Model Ideal Gas Viscosity - Sutherlands Gauge Presure - 0 Steady Density Based solver I'm quite confused why there is no variation in velocity contours or temperature at all, so any help would be very much appreciated. |
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