UDF of heat flux with respect to x direction on the surface of complex geometry in ANSYS Fluent
I am working on a school project and I am trying to analyze a single channel geometry in a regeneratively cooled rocket nozzle. On the hot gas side of the nozzle I have calculated the heat flux to the wall at discrete points from x=0 to x=length of nozzle.I want to apply these heat fluxes with respect to the x-coordinate on the inner surface of the nozzle. I currently have the tabulated data attached in a .txt file. Keep in mind this is not time varying it is only position varying and a steady state problem. Any help would be greatly appreciated!