Wouldn’t it be nice to have a standardized, digital repository of parameterized models frequently used for supporting design decisions? Wouldn’t it be even nicer to have these models developed, documented and certified by experts to conform to best practices? CAE Handbook powered by StressCheck® puts the power of numerical simulation in the hands of designers, engineers and analysts. Meet the FEA tool you have been waiting for.
A novel framework for Smart Engineering Simulation Apps.
CAE Handbook powered by StressCheck® increases productivity and serves as a repository for corporate design knowledge. A newly redesigned graphical user interface enhances the usability and functionality of the Handbook framework which is deployed as a stand–alone 64-bit desktop application. Fully supports Windows 7 and 8.
- Information document available for each solution with detailed model description and expected results.
- A simple and intuitive user interface to deploy solutions of much greater complexity than those available in traditional engineering handbooks.
- Solutions obtained with StressCheck®, verified by p-extension.
- Automatic reporting of results ready to be printed and archived.
- Built-in Results Viewer provides dynamic viewing of the FE mesh, contour plots and more.
- Supports the latest StressCheck® file formats (.scw and .scp).
- Framework for standardization or recurrent analysis tasks.
- Preservation and accumulation of corporate knowledge with increased reliability.
- Solutions created by FEA analysts and deployed for non-FEA experts.
- Consistent results produced by tested and approved analysis procedures.
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“A screening of existent commercial and non-commercial tools was carried out in respect to their fracture mechanics capabilities, their design abilities, implementation as well as their complexity. Although, there are many software possibilities, only those within the reach of the author were evaluated. This resulted in the selection of the commercial tool StressCheck®. The assessment of crack propagation on compact tension and two stringer specimens governed by the Paris and Forman regimes was satisfactory compared with experimental results using the material data from simple standard specimens.”
Lloren Llopart Prieto (EADS)Doctoral Thesis, "Modelling and analysis of crack turning on aeronautical structures"