Programmable mechanical responses of a hybrid star-rhombus honeycomb based on digital design method

S Wang, HT Liu, GB Cai - Thin-Walled Structures, 2024 - Elsevier
Hybrid honeycombs with programmable mechanical responses have received widespread
attention due to their multifunctionality and superior mechanical properties. To improve the …

Effect of geometric configurations and curvature angle of corrugated sandwich structures on impact behavior

I Bozkurt - Polymer Composites, 2025 - Wiley Online Library
The aim of this study is to numerically investigate the low‐velocity impact behavior of carbon
fiber reinforced orthogonal woven fabric composite sandwich structures with five different …

Material performance, manufacturing methods, and engineering applications in aviation of Carbon fiber reinforced polymers: A comprehensive review

X Xu, G Peng, B Zhang, F Shi, L Gao, J Gao - Thin-Walled Structures, 2024 - Elsevier
Carbon fiber reinforced polymers (CFRP) is becoming the predominant material in the
aviation industry due to its excellent performance including light weight, high specific …

Crashworthiness design and evaluation of civil aircraft structures

V Lopresto - Progress in Aerospace Sciences, 2024 - Elsevier
One of the most critical air transportation issues is the passengers' protection during collision
and impact events that must be absorbed in a controlled way in order to reduce damages …

A stochastic gradient estimate-based formulation for capturing the high strain-rate behaviour of a ductile target subjected to ballistic impact

A Kaithavalappil, S Sarkar - International Journal of Impact Engineering, 2025 - Elsevier
Investigating high strain-rate phenomena characterized by high-velocity impact is crucial for
designing protective structures. Such impacts cause rapid microstructural changes …

Experimental investigation on mechanical properties of the sandwich structure with orthogonal corrugated core reinforced by polyurethane foam

Y Deng, H Yu, J Li, Y Zheng, G Wei - Polymer Composites, 2025 - Wiley Online Library
The aim of this paper is to explore the effect of polyurethane foam filler on the out‐of‐plane
compressive property and low‐velocity impact resistance of the orthogonal corrugated …

Research of typical frame section of a fuselage against crash

Z Feng, B Wang, C Wang, T Suo - Journal of Physics: Conference …, 2025 - iopscience.iop.org
This study focused on a typical fuselage section of a certain type of civil aircraft. Optimization
of parameters such as the angle of floor-mounted columns, column structural forms, and …