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Getting fields exceded field length error while exporting. inp in Hypermesh
Hello all, I'm trying to analyse an aircraft wing model with Optistruct non-linear statics with "PARAM,LGDISP,1" and "PARAM,FLLWER,1", in order to simulate large displacement efects on the structure, namely wing crushing. No contact or non-linear material curves. I'm using the following non-linear parameters: NLPARM 100 10…
A few months ago, I asked three questions about the Panopticon dashboard. https://community.altair.com/discussion/62762/i-have-a-question-about-the-panopticon-screen-configuration-and-input-settings I tried again after updating to 2025.0.1 and the recently updated 2025.1.1, but issues 1 and 2 still persist. 1) When I add…
Dear Team, I wants know how to create AEFACT & MKAERO1 card and how it referrence to the model to the load step (because loads like AEFACT & MKAERO1 card did n't mentioned in load steps) ? And need more explaination about AEFACT & MKAERO1 cards how it works? i try to review it , but it did n't work! OS-T: 8030 Flutter…
i need a help to solve fatigue problem using displacement history data, i know how to define load history but not getting how to deal with displacement history data
Hello everyone , I am meshing a cooling plate . the cooling plate basically have two plates : a) channel plate b) base plate . Both the plates are brazed together I have meshed base and channel plate separately . How should i join both the plates to get real world scenario. I have attached an image with top plate as…
Contact 조건이 없이 Concentrated Load를 주고 해석을 진행 했습니다. Hyperview에서 Concentrated Load 에 걸리는 하중을 실시간으로 표시하거나, Plot으로 뽑는법이 궁금합니다. 도와주세요!
I’m a beginner with this software, so I’d like to ask not only about the issue but also how to use it. When clicking the "Comparison of Results" tab after performing structural optimization, the optimized result is displayed, but the displayed mass value is clearly incorrect. The optimization conditions were: Maximization…
Hi, I have been using the CCS wing meshing tool in FlightStream to create the wings and horizontal/vertical stabiliser for a light aircraft. The mesher works fine without control surfaces, but the moment I specify a control surface it seems to ignore any growth scheme settings. For example, this wing has 160 chordwise…
I did mesh a 1/4 of my solid, then did 2 mirrors, just like shown down there: Than the 2 mirrors so i can have the whole solid: I was exporting the file to another software to simulate, Abaqus. I did a simple test, the program identified that, and i get that warning "There are 4 unconnected regions in the model." And then…
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