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Found 626 results

  1. Hi, I extracted stiffness matrix using DMIG . How to identify the stiffness value of the node and direction and matrix size in .pch file? Pls refer the attached image for reference.
  2. Hallo, i want to convert an abaqus modell to an optistruct modell via the hypermesh convert makro. With most of the entities it works fine, but with some not. For example the section properties especially the beam section, connector section and solid section cards are not supported in conversion. The abaqus modell was build up in ansa and now I want to do a topology optimization in hypermesh optistruct. How can I handle this problem? Are there any configuration files for those or any other not supported cards and where can I find them? Thank you in advance. MT
  3. I am able to run analysis successfully with 0.2 MPa pressure. But it is giving an error if i increase the load to 0.22 MPa in the same model. What could be the reason? Change in NLPARM card parameter didn't help. .out file is attached. fuel cap.out
  4. Hello all, I have recently started exploring Fatigue and Modal Analysis in optistruct. I wanted to know if there is any User manual where meanings of different variables in cards are explained as in LS Dyna User Manual. Thanks in Advance.
  5. Yousif

    1d fem

    Hi could somebody please answer me on this page. Thank you
  6. I am creating flexible body in optistruct of a truck chassis with trailer which is very big model with so many number of nodes and elements. CBN method is used UB_FREQ given 20 but i am getting 131 modes and fbi file size is about 15GB which is too much to import in SIMPACK and then i gave NMODES 40 but still its giving 131 modes which is very high So please help me with this Thank You
  7. Hello, I'm currently trying to optimize the laminate of a cfk part with the free sizing optimization. At the end of the run it states "OPTIMIZATION HAS CONVERGED" "FEASIBLE DESIGN (ALL CONSTRAINTS SATISFIED)" but the programm is just reducing the mass while the displacement constantly gets bigger and is far bigger than the max displacement constraint I set for the optimization. The total displacement constraint is set to -2mm. Min ply thickness is set to 2mm and max 50mm.
  8. Dear All, @Prakash Pagadala in attached image green- housing yellow - shaft blue- ball ball makes a contact with shaft at 2 points and with housing at 2 points. at every contact there is an interference of 3 microns. housing is fixed and shaft is allowed to translate axially. i tried contact with static coefficient of friction and and clearance value but still groove surface of shaft and housing is penetrating the ball and vice versa. can anyone suggest how can i work on this??
  9. Hi, The problem consists of a connecting rod submitted to axial loads which define the phases of admission (traction) and combustion (compression). I am trying to run the following optimization:  2 load steps : Traction Compression 2 responses : Volume Compliance 1 constraint : 60% Volume 1 objective : Minimize compliance I managed to run a direct transient analysis for the two separate load cases. I tried running a topology optimization for one of the load cases but an error occured with the following message: *** ERROR # 557 *** DRESP1 2 is not referenced from within a static or an MBD SUBCASE. This type of response must be specified from within a static or an MBD SUBCASE. This error occurs in DESOBJ 2. I would like to know: How can I create alternating load steps to simulate the traction and compression phases If it is possible to run an optimization with these dynamic loads Thank you !
  10. Hey, how can I extract COG, Moment of Inertia and Mass as an output by running a static solution in optistruct? Thank you in advance.
  11. I am attempting this tutorial but I am confused regarding the solver manager. I have altered the fem file using the text editor, then saved it with the name: controlarm.fem.txt, which gives it the suffix of a .txt file. But the tutorial then says to run the file in the solver manager. This is a .txt file so it does not work in the solver manager. What am I missing? Kind Regards, Laurence Maskell controlarm.fem.txt
  12. Hello, I have set the DESMAX in the individual model files but when running the MMO it uses a default value of 80 iterations. How can I change this default?
  13. Hi , Is it possible to apply cyclic load in Optistruct Analysis? Regards, Arul
  14. I'am studying how a components performance is affected by the materials isotropic and orthotropic behaviour. The image attached shows the same 3d solid mesh using hexa and penta elements but with an isotropic material (top) and an orthotropic material (bottom). I'am using mat1 for isotropic and mat9ort for orthotropic. There is a clear difference in stress for the cpenta elements compared to the chexa. Are cpenta elements fully supported for mat9ort or is this behaviour a result of the cpenta element formulation?
  15. I am trying to run an example, provided by altair on their help page, about vibroacoustic interaction and wave propagation using infinite elements CACINF3. The link to the page is: https://altairhyperworks.com/hwhelp/Altair/2017/help/os/topics/solvers/acoustic_analysis_of_speaker_os_example_r.htm#results However, I am unable to run the problem using optistruct 2017. The error message given is: The model file follows attached. Speaker_IE-C.fem
  16. hello, i'm triying to to find a solution of a probleme i'v acoutred in the last few days, i'v exported from ANSYS a .cdb, file which i opened with hypermesh and while i'm on the Ansys user profiles every thing seems ok, i got all material propreties, geometri propreties, DOF... but the memont i pass from Ansys user profile to optistruct i lose all my data (no materials defined...), i got only the initial geometry. so i got three questions if anny one got the answers i'll be realy greatfull. 1) is there a way to keep all my imputs when i change the user profiles from Ansys to optistruct ?. 2) how can i define the following matairial propreties using optistruct?: * thermal expansion * permeability * resistivity (constant) * specific heat * thermal conductivity 3) how can i also define a COMBIN14 element type using optistruct? and thank you everyone
  17. Hello. I am working on the NL buckling of a composite panel (geometric NL implicit) and I successfully setup the model and ran the analysis within radioss after automatic conversion from the optistruct input. The problem is that although I specify I need 50 increments (NINC) with PW convergence criteria, the solution ALWAYS converges at 25 increments and of course the total buckling is not captured. Below is my NLPARM card from the .fem file. I am not specifying anything else in the NLPARM card or in any other cards. Can you please help? NLPARM 6 50 0.0 6 50 PW + 0.01 0.01 20 + 1.0 Thank you
  18. I'd like to share the seamless integration that Compose with other HyperWorks applications, such as HyperMesh and OptiStruct. In order to expose the Compose function to other HyperWorks applications, we need to register the function. This is done clicking on the right mouse button on Register Function in Compose: After this step, we may now see that the function has been registered under the same mouse click shown above under Show Registered Functions button. Once it is registered, we may now use it inside other HyperWorks softwares, and the function will be available without the need for closing and reopening the application of interest. Example in HyperMesh: Why Compose and HyperMesh? Matrix Browser queries and modifies HyperMesh and HyperView data entities without writing cumbersome TCL coding, along with a Math method developed in Compose. Example in HyperGraph: Why Compose and HyperGraph? Plotting capabilities of HyperGraph are expanded with Compose’s advanced functions and custom procedures developed by the user. Example in HyperView: Why Compose and HyperView? Advanced post-processing or special mathematical approaches may be applied directly on the model. Example in HyperStudy: Add a new output response Define a new expression Use your custom Compose function Why Compose and HyperStudy? User-defined functions to perform design exploration and optimization. Example in OptiStruct: Why Compose and OptiStruct? User-defined functions to perform optimization with DRESP3 card (desired response based on external files). Regards, Roberta
  19. hello, i want to define a anistripic material in optistruct and i don't know what card image should be used for such a material. thanks
  20. Hello, I'am optimising a front wishbone for both the left and right of a suspension. My idea is to have the loads and boundary conditions mirrored between loadsteps however there is a spring/damper element that would effect the results. Can you deactivate/ignore elements between the loadsteps? Or is there a better way to combine the optimisation so that the component is optimised for both the left and right tyre loads?
  21. Hi,I have a question, In Optistruct, how to apply a displacement load on a cylindrical rigid wall to simulate a three-point bending test like following picture? Thanks in advance。
  22. Hi , I am trying to restart from the end of a successful nonlinear analysis and append new nonlinear subcase with CNTNLSUB. I have included a new nonlinear subcase to the restart file, While doing so A fatal error has occurred during computations: *** ERROR # 4761 *** The restart model is inconsistent with the original one. Please compare the two input decks. Please help me to restart. Thankyou
  23. Essa linha clara são 4 elementos de viga que recebem uma força na vertical no centro deles, representam uma manga de eixo. O objetivo é analisar distribuição de tensão nas bandejas de suspensão, por isso é bem simplificado. O problema é que, com uso de RBE3, eles deformam dessa maneira aleatória. Agradeço desde já as respostas.
  24. Dear All, I am trying to do the tutorial of the rubber spring but when I am setting the analysis load step, I can't find the Analysis type Geom non linear (implicit) Is there something missing in my version of HW?
  25. Hi, I am a new user to Hyperworks. I am trying to analyse and optimize a composite monocoque chassis. I haven't gotten to the optimization part yet as I'm stuck trying to even run the analysis. Every time I try to run the analysis I get the following error: *** ERROR 14: Missing MAT # 3 referenced by PLY # 3, (existing MAT with this ID is of incorrect type). *** ERROR 14: Missing MAT # 3 referenced by PLY # 8, (existing MAT with this ID is of incorrect type). What I have done is that I have a symmetric stack of 2 layers of carbon fiber, aluminium honeycomb and 2 layers of carbon fiber. I have defined carbon fiber as MAT 8 and the honeycomb as MAT9ORT. The property I have specified for the geometry is PCOMPP. I have added pin joints to the rear suspension and a torsional load at the front suspension. I understand that another thread has been posted about this but I don't understand what the replies are telling me to do. Any help would be appreciated.
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