[syed123]

Hello,

I have been working on a project where i will be simulating flow over a nacelle (aircraft turbofan). I do not require simulating the exhaust flow as that is not the area of study, only the inlet region is required. (recreating a this research for my own project with my own engine nacelle geometry)

The Research Paper that i will be reproducing: https://citeseerx.ist.psu.edu/viewdo...=rep1&type=pdf

I am currently stuck on the meshing stage of the CFD as i now continue to get an error. The Error says "Patch-conforming tetrahedron mesh failed because of an edge intersection in the boundary mesh."


I am new to Ansys CFD and would appreciate if anyone can help me solve this error.

Thanks