I need to calculate the centre of pressure of an aerodynamic body using Paraview, with simulations having been run successfully in OpenFOAM. This is required in order to carry out structural analysis of aerodynamic device mounts.
Surely if the program is able to calculate the force on a body, it must assume a position where that force acts? Is this an output-able function in Paraview, or is there a way to calculate it?
It looks like the feature you are looking for is quite specific and will need to be implemented somehow.
Kitware could help you and implement it for you if you need it. https://www.kitware.eu/home