Hello all,
I am trying to simulate a small RC propeller in a duct to find the thrust generated at a specific rpm. The issue I am facing is that my results vary drastically depending on the size of the computational domain. Any ideas or tips on what I might be doing wrong would be much appreciated.
Thank you.
I am trying to simulate a small RC propeller in a duct to find the thrust generated at a specific rpm. The issue I am facing is that my results vary drastically depending on the size of the computational domain. Any ideas or tips on what I might be doing wrong would be much appreciated.
Thank you.