Aug 2026· Muthanna Journal of Engineering and Technology· 0 citations
Abstract
Thin-walled crash boxes are key energy-absorbing components whose geometry influences vehicle mass, impact-force transmission, and crash energy dissipation. Existing optimization approaches often rely on complex geometries or assess structural failure only indirectly, which limits their application to locally manufacturable steel components. In this study, an integrated framework that couples an ABAQUS/Explicit model with the non-dominated sorting genetic algorithm II (NSGA-II) is developed for a square steel crash box that can be produced with conventional manufacturing processes. Wall thickness, box length, trigger-hole diameter, and trigger-hole position were optimized to minimize mass and peak crushing force while maximizing specific energy absorption (SEA), subject to equivalent plastic-strain and connection-safety constraints. The baseline design had a mass of 4.25 kg, an SEA of 9.34 kJ/kg, and a peak force of 115.2 KN. The selected balanced Pareto-optimal design reduced the mass to 3.98 kg (6.4%), increased the SEA to 10.15 kJ/kg (8.7%), and lowered the peak force to 108.4 KN (5.9%). Its connection safety factor increased to 1.18, while the maximum equivalent plastic strain remained below the allowable limit of 0.35. Sensitivity analysis identified wall thickness and trigger-hole geometry as the dominant design variables. The proposed framework provides a practical route to improving crashworthiness using conventional steel and accessible manufacturing processes.
To address the failures observed in aluminum-alloy fuel tanks, specifically, cracking of the dual-chamber sealing partition, end cover, and drain boss, finite element analysis was employed for comprehensive calculation and structural optimization. Stress, strain, and displacement under varying load conditions were eval...
Hong Chi, Hai-Sen Lei, Liying Sun et al.· SAE technical paper series· 0 citations
Formula SAE regulations require every prototype vehicle to be equipped with an impact attenuator as a passive safety system capable of absorbing a minimum frontal impact energy of 7,350 J at an impact velocity of 7 m/s for a vehicle with a mass of approximately 300 kg. This study aims to design an impact attenuator tha...
A. Pratama, Zainal Abadi, Delima Yanti Sari et al.· Journal of Engineering Resea...· 0 citations
Reducing structural weight in commercial aviation is a primary challenge for efficiency. This study introduces a design framework optimizing a Fowler flap bracket using topology optimization (TO) tailored for additive manufacturing (AM) constraints. Rather than expensive fluid simulations, the methodology utilizes anal...
M. Bayrak, Okan Bakbak· Journal of Polytechnic· 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
This paper presents a systematic experimental and computational investigation of the free-vibration characteristics of a Laser Powder Bed Fusion (LPBF) AlSi10Mg thick-walled cylinder, a geometry relevant to electric-machine housings, hydraulic sleeves, and pressure-carrying components exposed to resonance-critical serv...
M. H. Shah, S. Hassan, L. Pešek· Applied Mechanics· 0 citations
The purpose ofthis study is to quantify how infill geometry affects the crashworthiness of fused filament fabrication (FFF) 3D-printed polylactic acid (PLA) tubular structures subjected to axial compression, with the aim of identifying an infill pattern that maximizes energy management and deformation stability....
R. Hasanzadeh· Rapid prototyping journal· 0 citations
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