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Hi everybody, I can't pass the boundary conditions of a 2D model to Ansys Workbench SCDM, even though I've defined inlets, walls, outlets with colors and imported Workbench by ACT APP.

Hello everyone I built a parametric propeller model using Caeses and imported it into the Workbench platform, meshed it with Fluent Meshing, solved it with Fluent, and I had a problem with solving failures. I named the propeller surface "wall_prop" and selected all the wall_prop named faces in fluent to establish the output as thrust and moment. However, whenever the parameter points are changed and the mesh is updated, the original name will become wall_prop_1, wall_prop_2...... the original name will disappear, and the output torque and force will not automatically select the new name, resulting in the calculated thrust and torque being wrong or the software directly reporting an error. I don't know how to solve this problem so that the automated simulation can continue.

Hi,guys， excuse me .I can't find the B-series propller in CAESES sample. How could get or design it ? I have to implement it in my project.Can you give me some advice or help with the B series? Looking forward to your reply. Thanks.

Hello everyone. I'm trying to import a CAESES model into Workbench, but the geometry cannot be imported into ANSYS Geometry. I have read the relevant tutorials in the software in detail. CAESES 4.4.2,Ansys Thank you very much for your reply! test.rar

I have three questions about CAESES、 workbench and propeller feature。 1、Import an existing STEP geometry in CAESES with units in meters and dimensions is 0.0046m=4.6mm, but when I import FSC into the workbench and opening it through SCDM, the size has changed to 0.0046mm. The size has been reduced by a thousand times. How to correct it? 2、After importing geometry A into CAESES on the workbench platform, it is necessary to performExternal flow CFD analysis on A. Therefore, an external computational domain was created using SCDM in the A-3 module to form B. when the parameters of CAESES were modified, and the geometry in the A-3 module became C, but SCDM did not automatically create an external computational domain for it. So my question is, if in the optimization process, it is necessary to automatically create external computational domains for parameterized geometry, what should be done? 3、A propeller was created using CAESES' propeller feature. Since CFD calculation requires a closed geometry。 how can the tail and tip of the blade be closed for CFD calculation?