I am trying to do a CFD simulation of my UAV. the simulation is of incompressible flow with a flow velocity of 20m/s. Simulation completed successful there are no error.But, in postprocessing when i am trying to get pressure distribution on the surface of the UAV. Instead of get a colour gradient of pressure i am getting a solid colour. Is there some thing that i am doing wrong? if yes, please let me know
I think a slip-wall should still produce a pressure/force distribution over its surface. Still, you do need to follow @mgiannios fix and set walls to no-slip. I’m not sure if SimScale has already included the capability of integrating the pressure over a surface, but if not, check out this link and do it in Paraview
the issue with the post processing is that some “bad cells” with really high values exist, and they “drag” the full range of the scale. As a result, the normal values are all colored in blue.