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The success of the transition and the mapping of the Loads & Boundary Conditions (LBCs) can be checked in the Map LBC tab. All newly created LBCs and their status are listed. If a LBC was not created successfully, the LBC can be manually adjusted by double clicking on the LBC.
With the green check mark checkmark the mapping can be confirmed:
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The whole project will be converted to a MSC Apex project. A copy for MSC Apex Generative Design will be remainedpreserved.
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The geometry as well as the LBCs and Material information are transferred and available for the verification.
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The optimised geometry needs to be meshed with a tetraeder tetrahedral mesh for the reanalysis. For the Jet Engine Bracket a quadratic element with a mesh size of 3 mm is chosen.
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For the reanalysis in MSC Apex a 3D Element Property needs to be created. The corresponding Material ID with the used material (in this case: Titanium) needs to be selected.
If anisotropic material was is used in the optimisation, a material coordinate system needs to be selected. In this case, create a new / correct one for your anisotropic material orientation.
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Assign the 3D Element Property to your mesh (not to the solid):!
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Step 5: Set up the static scenario
In the studies tab the static analysis scenario can be set up. Therefore, the model representation need needs to be linked to the optimised geometry. Under Loads & Constraints the Events can be set up.
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