HyperSizer Express appears highly automated and easy to use as well as something you can use from the early stages of a design project. This provides the flexibility for designing stiffened panel bays with stiffeners that have varying dimensions and materials. Incidentally, it works with models from pretty much any FEA (finite element analysis) system such as Abaqus or OptiStruct and it works seamlessly with high-end HyperSizer. 379Download Part 1 – 1 GBDownload Part 2 – 1 GBDownload Part 3 – 62 MBDownload DS CATIA P2 V5-6R2020 SP2 x64 UpdateDownload Part 1 – 1 GBDownload Part 2 – 397 MBDownload Part 1 – 1 GBDownload Part 2 – 1 GBDownload Part 3 – 6 MBDownload DS CATIA P3 V5-6R2019 SP4 x64 UpdateDownload Part 1 – 1 GBDownload Part 2 – 373 MBDownload Part 1 – 1 GBDownload Part 2 – 960 MBDownload Click This Link CATIA P3 V5-6R2018 SP6 UpdateDownload part 1 – 1 GBDownload part 2 – 1 GBDownload part 3 – 1 GBDownload part 4 – 12 MBDownload DS CATIA DELMIA-ENOVIA V5-6R2017 SP6 UpdateVersion 2016:Download DS CATIA P3 V5-6R2016 GA (SP0) x64Download DS CATIA DELMIA-ENOVIA V5-6R2016 SP6 UpdateDownload DS CATIA P3 V5-6R2016 DocumentationVersion 2015:GA (SP0)32-bit editingDownload part 1 – 1 GBDownload part 2 – 734 MB64-bit editingDownload part 1 – 1 GBDownload part 2 – 813 MBService Pack 6Download 32-bit version – 616 MBDownload 64-bit version – 737 MBDocumentationDownload part 1 – 1 GBDownload part 2 – 121 MBfollow on facebook
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follow on Reddit. Examples of such data include sample calculations, margins of safety, critical load cases, analysis traceability details, material properties, and 2D maps (data in terms of stringer-bay coordinates).
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All Rights Reserved. Use HyperSizer to standardize your companys analysis with best in class verified and validated methods. Cross sectional geometry of stiffened panels are simultaneously optimized with the laminates’ ply stacking sequences or metal sheet thicknesses while considering manufacturing constraints. Its huge in aerospace applications. A simplified description of the workflow is that you load your FE (finite element) model, tell it what material you want, specify your failure and design criteria as well this website set other details. ST-SIZE was developed by a team of engineers working on the National Aerospace Plane X-30.
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”Tighter coupling to FEA optimizes product behavior analysisExpress is even more tightly coupled to FEA programs, such as NASTRAN and Abaqus, than the Pro version is. DirectX graphics features allow HyperSizer users to post-process analysis results such as margins of safety, controlling failure analysis, controlling load case, and ply-by-ply stresses and strains for the controlling ply and for the outer and inner most plies. • Standard and consistent use of approved analysis methods
• A corporate material database containing your company’s approved allowables
• FEA load extraction of thousands of load cases, and identifying critical load conditions
• Sizing metal and composite parts daily, with discretely meshed models
• GFEM updating and management of hundreds of files
• Data exchange with master parts dimensions spreadsheets including laminate ply schedules with CAD such as CATIA How to deploy a stress framework?
1) Develop Analysis Plugins of company’s methods
2) Establish a process to use the material database consistently from FEM assignment to HyperSizer failure predictions
3) Deploy Work Packages of margin policies, user roles, and project setup
4) Setup aircraft specific GFEM Element Mapping to identify structural skin, stringer, frame segments to size structure and assign margins to parts not to finite elementsThe ultimate software tool for composite analysis structural sizing. com
Source: HyperSizerAre you looking to finance your project, product or idea? Contact us for supportWho can have a cooperation and a partnership with us?SMESs COMPANIESRD LABSRESEARCHERSINVENTORS EVENTS ORGANIZATIONSCookies© Haptic.
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“Tight FEA coupling is key for the types of mechanical response analyses an see it here would carry out with Express,” says Collier. HyperSizer ensures structural integrity through failure analyses. Hit todays Pick of the Week link to start. 34 Other solvers are supported such as I-DEAS. Express will effectively optimize the frame for these kinds of deflection limits, with fabric and unidirectional layers, to determine that best shape and location of the individual plies as well as the best orientation they should be placed in. .