# hubéry10

Members

17

• Rank
Beginner

## Profile Information

• Country
Germany
• Are you University user?
Yes
1. ## Hyperview student

thank you guys now everything works fine
2. ## Hyperview student

it is strange but now it´s working. But i have another problem, where can i select the loadcases and where can i hide or show components? Normaly it´s in the left toolbar but there is nothing
3. ## Hyperview student

Hi i've downloaded the student version of hyperworks so hypermesh is running fine but I cannot not see the results in hyperview. Can somebody tell me why , because in the description of the student version is nothing written. Or can someone tell me an open source viewer.
4. ## Give solid a eigenfrequency

Hi, is it possible to give a solid a defined eigenfrequenzy. The Problem is i had to do a modal Analysis of a satellite structure and the first eigenmode had to be above 40Hz, but my tank had a eigenmode at 30Hz. But i know that the frequqnzy of the real tank is 45Hz. So can i give the solid a eigenfrequency with 45Hz? Thanks for your help
5. ## How to see stresses in the plies of a laminate

ok now everything is fine, it runs with the global request output file. But i have two more questions. - What´s the difference betweeen Composite Failure and Composite Failure Index - And the difference between Failure INdex and plies with Maximum FI Thanks for your help
6. ## How to see stresses in the plies of a laminate

thanks for your offer but now i solved the Problem. i had to write cstress and cstrain in my loadcases. for better understanding see the Picture below the first is the old the second the new. I highlighted the lines i changed.
7. ## How to see stresses in the plies of a laminate

thanks for the informations, now i edit my .fem file like shown in the picture, so it works and i have failure Output for each ply. But the Problem is have no stress Output for the plies only for the Composite. But i need the stresses for each ply, because i want to calculate my failure by hand. I hope the pictures show what i mean.
8. ## How to see stresses in the plies of a laminate

Thanks for answering i found CSTRESS; CSTRAIN but no CFAILURE I use PCOMP. What does the (G) means? If relevant I am using Hypermesh 13
9. ## How to see stresses in the plies of a laminate

Hi, i built a model with Laminates, so how can i see my stresses in the plies. I want to know my stress in the facesheets and the honeycomb plie. Thanks for answering, hubéry10
10. ## different connectors

Hi guys, can someone say me what are the properties of the different connectors. Or give me a link where they are discribed, sadly i found nothing in the Help or web.
11. ## How to simulate failure theory of laminate

I selected SOUT in PCOMP and have Input ST, SC, SS(MAT1) ; Xt, Xc, Yt, Yc, S(Mat8) but CFailure is not presented. So whats my mistake?
12. ## How to simulate failure theory of laminate

ok thanks and where can i find the failure indices?
13. ## How to simulate failure theory of laminate

Hi, i built my model in hypermesch with shell elements, this elements have a PCOMP property with three layers. So how can I simulate wheter the Shell elements are safe or fail? I found a Website http://altairatc.com/europe/EHTC2011-Abstracts/EHTC-Presentations-2011/Session_12/AgustaWestland_presentation.pdf and there they talk about a Skript called HM_PE.tcl. So where can i find this Skript or is there any other Analysis i can make? Kind regards
14. ## delete part of contact surface

Hi guys, i want to contact the red Shell component with the Grey solid. I´ve don this with the tool autocontact. The Problem is i want to delete parts of the green contact surfs, can someone tell me how. In the Pictures attached i marked the surfs i want to delete with a blue dot. Thanks for answering.
15. ## How to design a honeycomb sandwich plate

should i leave the other entries blank in mat8, or schould i put in dummy values like 1 for E2, G2Z...
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