Jump to content

Premanand Suryavanshi

Members
  • Content Count

    376
  • Joined

  • Last visited

  • Days Won

    6

Everything posted by Premanand Suryavanshi

  1. Hi Nes, I think you have given a wrong file. Because i see different model when i open your file (as shown in below image). Please can you check and share the correct file. Thank you
  2. Hi vishruthdilip This is been already answered to you, in your previous query. Please can check that. Thank you
  3. Hi STEz3ro2, Please can you explain what you are trying to do? share some screen shots and will help you to solve your problem. Thank you
  4. Hi Nishanth Please refer below Tutorials. I think this will give you an idea how to setup for optimization. If you still have any doubts , let me know. OS-T: 2030 Control Arm with Draw Direction Constraints OS-T: 2095 Frequency Response Optimization of a Rectangular Plate Also for more details you can refer to our optimization eBook. Please download from below link. https://altairuniversity.com/free-ebooks-2/free-ebook-practical-aspects-of-structural-optimization-a-study-guide/ Thank you
  5. Hi Capet16, I think there are duplicate elements created. Please can you check. Thank you
  6. Nes, Under combine through option, select all internal faces and try. Thank you
  7. Hi Imre, I think you need to model it with solid elements only. But, i don't think you can perform Rupture analysis of composite plate in Radioss (it will not support). Thank you
  8. Please find the files below load1.csv load2.csv
  9. Hi akash@1995, Dof1, 2, & 3 are translation degrees of freedom in x, y, z direction respectively. Similarly dof4 , 5 & 6 are rotational degrees of freedom in x, y , z direction respectively. If dof2 is selected, it means that you are constraining translation movement in the y direction. Orientation determines how springs are oriented in 3D space. Click the switch and select from either node, vector, and components. • Node: Select a node to specify the vector orientation. • Vector: Use the standard plane and vector selector to determine the orientation of the spring. • Components: To be used if the direction of the local y axis of the spring is to be specified by typing in the X, Y, and Z components. Thank you
  10. Hi Nes, I'm able to do union of two solids (A+B). Please can you show me what is error you are getting? Thank you
  11. carlosmarbo, But i don't see any material system in your images. I see only global system. Have you created material system? Please refer below video for Composite modeling. Thank you
  12. Hi sanket Please follow below path HyperWorks Desktop Reference Guides Overview > HyperWorks Desktop Reference Guide > Programming with Tcl/Tk Commands > Tcl/Tk Commands > HyperView: Thank you
  13. Here is the model. altair_knuckle.hm Thank you
  14. Hi carlosmarbo, For an An-isotropic material we need to define separate systems at many level. I found a script for that, which i have attached in my reply, with a video which helps you to understand how it works. I hope this helps you anisotropic_layering.tcl anisotropic_layering.mp4 Thank you
  15. Hi Imre, Please refer below post. It is similar to your issue. I hope it helps. Thank you
  16. I see that thickness of the structure is less. So, i think you can take a mid-surface of this and go for shell mesh. Also refer below post for more details. Thank you
  17. Hi carlosmarbo, Plies will be oriented with respect to material system. But, make sure while creating the plies you select the material system every time you create a ply. you can compare it straightaway. Thank you
  18. Please can you show me the honeycomb structure with few images. Thank you
  19. Yes Q.Nguyen-Dai is right. These are two different formats. It may not open in work bench. Thank you
  20. Hi vishruthdilip, You are right. You need to create a 3D cad model for honeycomb structure and use appropriate material(MAT9/MAT9ORT) and properties(PSOLID). Thank you
  21. It means 1N is the total load and it will be distributed to all the nodes. Example: if 1N load is applied using RBE2 and there are 10 nodes. This implies 0.1N load on each node. Thank you
  22. Hi Zdeny, Goto File > Eport > solver deck > in the file selection, change file type to Ansys and Template also to Ansys and click Export. Thank you
  23. Hi Please can you check material orientation panel in Aerospace user profile. Where you can define the orientation by curve. Thank you
  24. Hi Pedro Neves, I think it might be because of your system configuration. We are able to run it quickly at our end. Please can you tell us which version of Solver you are using and configurations of your system Thank you
  25. Hi imranshaik1432u, Please delete settings files and try again. If you face same issue even after doing it, please share us your file and will check it. To delete settings files please follow below post Thank you
×
×
  • Create New...