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March 12, 2021, 22:05 |
Mesh Errors for an Turbofan Engine
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#1 |
New Member
Join Date: Mar 2021
Posts: 2
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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 |
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ansys, cfd, fluent, mesh, nacelle |
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