This research examines the reliability of BIM-to-FEM transfer procedures using Autodesk Revit and CSI ETABS by systematically evaluating native API-mediated and IFC-based approaches to show that BIM-to-FEM interoperability is still a somewhat automated process that needs rigorous verification.
Banothu Sairam, Nayak, A. V. Anjani Devi et al.· 0 citations
Given the demands of contemporary technology, as well as the complexity and diversity of manufacturing due to the quick updates of products, the traditional design of cotter joints has become inappropriate. One useful tool in this regard is computer-aided design (CAD) of cotter joints. Initially, finite element analy...
Farah Kamil, Maher Rehaif Khudair, Hameedah Sahib Hasan· International Review of Appl...· 0 citations
The structural design and optimization of an industrial lift platform through the application of composite profiles, specifically sandwich structures, to enhance performance characteristics compared to conventional metallic (steel)designs. The primary goal is to significantly reduce the platform's overall weight withou...
Mayur S. Awale, S. Gawade· International Journal of Adv...· 0 citations
Advanced analysis has been shown to improve material efficiency in statically indeterminate steel-framed structures compared with member-based linear elastic design methods. However, limited research has investigated its applicability to geometrically nonlinear steel structures where residual stresses are induced by th...
Eva Gurtata, F. Tahmasebinia· Applied Sciences· 0 citations
Composite materials have become widespread for use in aircraft load bearing structures due to their ability of reducing structural mass without compromising the required stiffness, strength and safety requirements in the face of aerodynamic, inertial and thermal service loads. This work has addressed with success the d...
Hao-Ming He· SAE technical paper series· 0 citations
In this work, an integrated aero-structural methodology is presented, combining a MATLAB panel-method aerodynamic solver with ANSYS finite-element analysis to predict the performance of a tapered NACA 2412 wing. The pressure distribution obtained from the panel method gave good agreement with CFD data, with a maximum d...
M. K. Abbas, T. Elsonni, Mokdad Hayawi Rahman et al.· Advances in Science and Tech...· 0 citations
We use cookies to run the site and, with your consent, for analytics and to show ads.
See our Cookie Policy.