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Found 77 results

  1. Hello guys, I'm currently optimizing a cfrp monocoque for our formula student team. After the free size optimization I wanted to check the composite failure, but I can't find cfailure in the control cards as it was in the previous version. How can I get results for the composite failure in Hyperworks 13 to look at in HyperView? Thanks in advance.
  2. Hello, I have a doubt, and I was wondering if someone here could help. I am setting up a Direct Frequency Response Analysis, and I want to set an oscillating load. I've read the documentation and some tutorials, however, I can't find the solution. The load I want to apply is: force (time)=A+B*cos(wt) A and B are constants, and w is the angular frequency. If A=0, the proccess would be (I think): - Set a unit load in the given direction, with load type DAREA, and magnitude 1. - Set a TableD1 load collector, with a range of frequencies and y=B - Set Freqi and Rload2 load collectors, and a freq resp (direct) loadstep accordingly. (I would be grateful if someone can confirm that is correct) However, when A is not zero, I have no idea what I should do. One more thing, is there a way to view the applied load in Hyperview? If there was, I could see for myself what I am doing. EDIT: I think I found a way to do this, with the global output request OLOAD, not sure it it'll work though. Thanks for your attention, hope someone can help! Regards
  3. Hi! I wanna model the rotation of a gear (wheel) with a preload in the pinion. I asume the preload is modeled with a moment but, how do I model the rotation? And which analysis type should I choose? (I don't want a quasi-static one). Some analysis don't let me include a LOAD. Thanks in advance!
  4. Using Hypermesh 2017, and User Optistruct. I have been trying to get the contour plots of a chassis both modeled with a beam model and a shell model to match up but the deflections of the shell model are always about 2 times as large. It should also be noted that the deflection images are nearly exactly the same with the same deflection trends but just the magnitudes are different. The following conditions are the exact same for both: forces, location of forces, constraints, overall size, thickness and material. The only conditions that are different would be the properties as the beam model is modeled with a PBEAM and assigned the correct beamsection while the Shell model is modeled with a PSHELL card and then assigned the thickness. Are there any common errors that would be able to describe why the beam model has almost exactly half the deflection of the shell model? Thanks for any Help , reply if more info is needed. Nicholas C.
  5. How can I perform a thermal analysis of a brake disc in Hyperworks? Guide me through some tutorial if possible.
  6. Hello all ! This is my first post here, I'm a student doing my master thesis in Mechanical engineering. Here is my issue, I successfully did the tutorial in order to realize dynamic explicit analysis with the "full car" model available in Hypermesh database and also the " Example 51 - Optimization in RADIOSS for B-Pillar (Thickness optimization) " in order to understand how the ESL method works. The next step is to optimize the car crash box using he ESL method, my aim is to optimize the component called " COMP-PSHELL_1 " by Thickness optimization. I wrote the .radopt file but I encountered an issue with the .fem file. See below the error, I was not able to solve the issue. *** See next message about line 14864 from file: fullcarv5.fem "CONTACT,3,3,0,3" *** ERROR # 1000 *** in the input data: Incorrect data in field # 4. See attached the .radopt, the engine/stater file and the .fem file Thanks for your help ! Aub N. fullcarv5.fem fullcarv5.radopt fullcarv5_0000.rad fullcarv5_0001.rad
  7. Hello, I'm currently attempting to do a study in which I created a simple square mesh. A pressure is applied perpendicular to the entire surface and the geometry is constrained along two parallel edges of the square. I'd like to observe the change in element displacement as the thickness varies. Is there any way to do this by parameterizing the thickness within the PSHELL component? I have attached an image of the setup to clarify.
  8. Hello Getting a problem in analysis, my 3D geometry goes into single plane during analysis.
  9. The 4th European Altair Academic User Day on June 26th (during the European Altair Technology Conference, June 26th - 28th in Frankenthal Germany) provides students, teachers, professors and researchers across Europe to network and share their experiences with Altair’s CAE solutions. Join us to hear how ESAComp assists schools and universities offering composite engineering courses, both in the class room and for post-grad research. Register here -> http://www.altairatc.com/EventPage.aspx?event_id=89&name=Academic+Day+2017 ESAComp-EDU-06-2014.pdf
  10. During analysis, I cant able to find Bulkdata option in Radioss. If I choose option other than Bulkdata, In "analysis" menu panel, Loads and Constraints option hides. Thank you in Advance
  11. Throughout JEC World show, come and see ESAComp in action with our engineers. With the launch of ESAComp 4.6, we'll show you the new capabilities, including Python scripting; enhanced panel analysis with shell modelled stiffeners... ESAComp now provides structural analysis of thick-walled pressure vessels from winding patterns imported from Composicad filament winding simulation. For HyperWorks users, ESAComp provides fully integrated solution for pre- and post-processing of composite structures, allowing ply-by-ply investigation of failure modes using advanced failure criteria. We're an active member of Altair Partner Alliance, find us together with Altair Engineering in Hall 5A on Stand N68
  12. When trying to calculate (solidification) with sleeves I get an error message: Error when preparing data for analysis (Domain error: Argument not in valid range) The calculation is O.K. without sleeves. Please advise.
  13. I've been recently working on a Knee joint model . I need to find the contact force vector between two particular components. I have been getting a lot of errors and unable to run the model. All the contact pairs and properly defined and I am able to generate all typical outputs except for contact output. please help me out. The output blocks defined so far are node and element outputs for all 8 components defined. Thanks in advance!
  14. I have designed a patch antenna which is operated using proximity feed. After running, in POSTFEKO the realised gain was very low despite "good" gain values. When I checked the current activity using Currents requests, I found out that only a little current is induced in the patch. I'm running FEKO 14. I have no idea what's wrong. Any help will be appreciated. Thank you.
  15. Hey everybody, I'd like to know if there is a way to display some sort of force vectors to visualize the force flux. My idea is to run the analysis mode and then being able to display where the actual force "moves along" the analyzed structure. This is important for complex structures to have a better understanding of why something might fail. With this in mind I'd be able to design a more evolved Designspace etc. Thanks for your help, Asaad
  16. Hi We are doing a car impact analysis against a pole (created as a rigid wall - Geometry type = cylinder). The simulation is running, but the impact only affects the front part of the car, it does't transmit the impact energy to the entire car. We think that we are missing to make a contact between the entire car, but we don´t know how to do it. As you can see in the second image, the front part of the frame, goes through the base of the car.
  17. what is meant by all the stress options we get while analysis of 1d beam element for torsion. for example CBAR/CBEAM LONG. STRESS SAC
  18. Hi Everyone, I was performing on my model through creating Stress-Strain curve and putting data values as per the curve given below. I have used NLPARM in Load Step. The error it is showing is quoted as : "The plastic material data specified on the TABLES1 bulk data entry ID=5 is invalid. The slope after the initial yield point is not less than the Young's modulus. ( 1.468927e+005 >= 1.550543e+005 ) at the segment 2. " I got, that the slope after the initial yield point should be less than the young modulus. So, I have ensure that very carefully in my curve but also it is showing the same error. Kindly clear my doubt as if I am doing something wrong. Thank you for reading and for answering. Enclosure: In the curve I have selected the first curve among all the curves.
  19. Hi! I wanna model the rotation of a gear (wheel) with a preload in the pinion. I asume the preload is modeled with a moment but, how do I model the rotation? And which analysis type should I choose? (I don't want a quasi-static one). Some analysis don't let me include a LOAD. Thanks in advance!
  20. Hi! I wanna model the rotation of a gear (wheel) with a preload in the pinion. I asume the preload is modeled with a moment but, how do I model the rotation? And which analysis type should I choose? (I don't want a quasi-static one). Some analysis don't let me include a LOAD. Thanks in advance!
  21. Hi everyone, how it is possible to define the /INISHE/ORTH_LOC card? I can't find the option to define correctly it. I need to initialize the orientation of an orthotropic material (that's defined as a P9 shell property). Thanks
  22. Dear all I need to know how to use connect for weld condition. Do you have any example or method for use this function ? such as : Arc welding or Seam welding ?
  23. Hi, First time using HyperMesh and I am following a tutorial for topology optimisation. The tutorial I am following is on pages 25-36 in the link provided. When I click OptiStruct, I do not get a message. When I click view.out, I get a message saying: '.out file does not exist.' Where am I going wrong? Thanks Laurence OptiStruct_11.0_Tutorials_(1).pdf
  24. I need to find the total strain energy of each component in my FEA model. Is there any tutorial about it?
  25. Composite structures all have joints, so their design and analysis is paramount to determining their overall performance. Therefore, ESAComp has comprehensive capabilities for both bonded and mechanical joints which are very efficient in the preliminary design of various joint configurations. Read more -> http://innovationintelligence.com/dont-come-unstuck-designing-structural-adhesive-bonds/ www.esacomp.com
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