Mesh Joining Problem with Turbomachinery Module
Posted: Tue Mar 28, 2017 12:59 am
Hello,
I have been trying to join two meshes with the transient turbomachinery module for the past week, but I can't get past 10 iterations before there is a mesh joining error. I made sure the interface of the two meshes matched and the mesh was equally distributed in the theta direction. In the radial direction, the mesh is grouped together near the wall, but the largest aspect ratio is no greater than 10. I have tried changing joining tolerance from 0.05 to 0.5, but see no improvement. I have also changed the mesh distribution in the radial direction to be matching and non-matching along with the overall distribution. Would changing any settings with cs_join_set_advanced_param effect the joining? Attached is the error mesh file and images of the interface.
Note, at the beginning of the computation, I copy, rotate, and join the mesh to make the full compressor. I have no problem with the mesh interface between the impeller and diffuser, only the interface between impeller and inlet. I can run my computation with the impeller and inlet domains static with respect to one another. For this case, I use a tolerance of 0.2 and an angle of 25 degrees.
Regards,
Andrew
I have been trying to join two meshes with the transient turbomachinery module for the past week, but I can't get past 10 iterations before there is a mesh joining error. I made sure the interface of the two meshes matched and the mesh was equally distributed in the theta direction. In the radial direction, the mesh is grouped together near the wall, but the largest aspect ratio is no greater than 10. I have tried changing joining tolerance from 0.05 to 0.5, but see no improvement. I have also changed the mesh distribution in the radial direction to be matching and non-matching along with the overall distribution. Would changing any settings with cs_join_set_advanced_param effect the joining? Attached is the error mesh file and images of the interface.
Note, at the beginning of the computation, I copy, rotate, and join the mesh to make the full compressor. I have no problem with the mesh interface between the impeller and diffuser, only the interface between impeller and inlet. I can run my computation with the impeller and inlet domains static with respect to one another. For this case, I use a tolerance of 0.2 and an angle of 25 degrees.
Regards,
Andrew