Training:
Relevant data for this tutorial:
Step 1: Transfer Design Candidate & Map LBCs and Material
For this Tutorial the Jet Engine Bracket project is used.
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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.
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Save the project and close MSC Apex Generative Design.
Step 2: Open Database in MSC Apex
Open the MSC Apex Generative Design database with the transitioned Design Candidate in MSC Apex.
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The whole project will be converted to a MSC Apex project. A copy for MSC Apex Generative Design will be automatically createdpreserved.
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The geometry as well as the LBCs and Material information are transferred and available for the verification.
Step 3: Meshing
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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Step 4: Assign 3D Element Properties
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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The scenario can also be expanded to include loads and functionalities unavailable in MSC Apex Generative Design to verify the Design regarding these conditions.
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