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I got this result from EDEM-motionview coupling. The boundary condition is a constant force on drilling head. How can I gain the total resistance backward on the drill head and body separately. And the resistance movement on the drilling head.
Is it possible through motionview itself, hypermesh or other softwares? I need to transfer a complex model from other group's work, so it is necessary.
I was wondering if there's a simple Tcl command to get the coordinates of the material orientation vector of an element, just like hm_getelementnormal *reviewmaterialorientation actually reads this vector before plotting it but I'm struggling to access its coordinates. Thanks in advance!
I am currently working on a project involving the "OS-T: 1500 Nonlinear Implicit Analysis of Bending of a Plate" and I am in need of the model associated with this task for practice. Unfortunately, I have been unable to find a reliable source for this model online and would greatly appreciate any help or guidance you could…
An online license was granted to our school team by Altair. I created my altair one account by following the license steps, but when I try to activate the license with my gmail account and password at the last stage, I am not successful, can you help?
Hello, Is it available to have the concepts (clusters) in generative design via the student bundle?
hello, I just started with simsolid. I did a study and it shows the max von mises stress on a seam weld location. Can I increase the solver adaptability on the weldment? I was able to create a group for the part on which the weld sits on for increased solver adaptation; but was not able to select the weld itself. What can…
Hi, I have this error when running my analysis. *** ERROR # 4966 *** Minimum time increment reached, analysis aborted. I tried to adjust the minimum time increment from 5e+06 to 5e+07, but the analysis took the entire night to run only 0.5%. And in the *nl.out flie, it shows the analysis failed with "element distortion".…
Hello, I need to create two types of meshes of a NACA 0012 airfoil in 2D. I have the airfoil and the boundary within which to create the mesh, but I can't divide the two surfaces to create the mesh. Can you help me? I'm using HyperMesh CFD Thank you
PBS101 - Foundation Course on PBS Pro Certification 3: Site specific Customization using Qmgr / Quiz
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