A theoretical model of honeycomb material arresting system for aircrafts

DOI10.1016/J.APM.2017.04.006zbMath1480.74241OpenAlexW2605234984MaRDI QIDQ2293868

Xianfeng Yang, Yun Xing, Jia-ling Yang, Yu-xin Sun

Publication date: 5 February 2020

Published in: Applied Mathematical Modelling (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/j.apm.2017.04.006

zbMATH Keywords

honeycomb materialenergy absorptionarresting systemcivil aircraftTHIMM

Mathematics Subject Classification ID

Impact in solid mechanics (74M20)

Uses Software

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Cites Work

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• The out-of-plane compressive behaviour of woven-core sandwich plates
• Modeling and adaptive control of magneto-rheological buffer system for aircraft landing gear
• Analysis and homogenization of functionally graded viscoelastic porous structures with a higher order plate theory and statistical based model of cellular distribution
• AN APPROXIMATE ANALYSIS OF THE COLLAPSE OF THIN CYLINDRICAL SHELLS UNDER AXIAL LOADING

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