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AI ELECTRICAL CIVIL AND MECHANICAL ENGINEERING

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
Open access Sep 2026

Design and analysis of a cotter joint using finite element analysis

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 · 0 citations
Open access Aug 2026

Structural Design and Optimization of an Industrial Lift Platform Using Composite Profiles

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 · 0 citations
Open access Aug 2026

Optimal Design of Geometrically Nonlinear Steel Structures Using Advanced Analysis

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 · 0 citations
Open access Sep 2026

Design and validation of lightweight composite load-bearing structures for aircraft using topology optimization and multiscale verification

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 · 0 citations
Open access Oct 2026

Integrated one-way aero-structural analysis of an aircraft wing using a MATLAB-based panel method and finite element analysis

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. · 0 citations

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