Numerical Investigation into In-Plane Crushing of Tube-Reinforced Damaged 5052 Aerospace Grade Aluminum Alloy Honeycomb Panels
| العنوان: | Numerical Investigation into In-Plane Crushing of Tube-Reinforced Damaged 5052 Aerospace Grade Aluminum Alloy Honeycomb Panels |
|---|---|
| المؤلفون: | Marjan Dodic, Younes Djemaoune, Branimir Krstic, Daniel Radulovic, Stefan Rasic |
| المصدر: | Materials Materials, Vol 14, Iss 4992, p 4992 (2021) Volume 14 Issue 17 |
| بيانات النشر: | MDPI, 2021. |
| سنة النشر: | 2021 |
| مصطلحات موضوعية: | Technology, Materials science, chemistry.chemical_element, finite element analysis, Article, Aluminium, Honeycomb, 5052 aluminium alloy, General Materials Science, Tube (container), Composite material, energy absorption, Microscopy, QC120-168.85, in-plane compression, QH201-278.5, Engineering (General). Civil engineering (General), Compression (physics), Finite element method, TK1-9971, Descriptive and experimental mechanics, chemistry, crashworthiness, aluminum honeycomb, Crashworthiness, Electrical engineering. Electronics. Nuclear engineering, TA1-2040, Deformation (engineering) |
| الوصف: | This paper aims to investigate the crashworthiness performance degradation of a damaged 5052 aluminum honeycomb panels under in-plane uniaxial quasi-static compression and the possibility of improving it using reinforcement tubes. The in-plane crushing behaviors and energy absorption capacities of the intact, damaged, and tube-reinforced damaged panels with different damage sizes in both X1 and X2 directions are numerically simulated by using the nonlinear FE method Abaqus/Explicit, and the crashworthiness performances are compared with each other. The validation of finite element model involves comparing the obtained simulation results with theoretical and experimental ones. Very good agreement between numerical, experimental, and theoretical results is achieved. The first maximum compressive load and the mean crushing load of the different honeycomb configurations are analyzed and compared through the load–strain curves. The energy absorption capacity of the damaged and the tube-reinforced damaged panels is calculated and then compared with their corresponding intact ones. The deformation modes are explained in detail. The obtained results show that the crashworthiness performance degradation is directly proportional to the damage size as well as the insertion of reinforcement tubes considerably improves in-plane crushing resistance of damaged honeycomb panels. |
| وصف الملف: | application/pdf |
| اللغة: | English |
| تدمد: | 1996-1944 |
| الوصول الحر: | https://explore.openaire.eu/search/publication?articleId=doi_dedup___::43281084ccc8b854546befe195da988fTest http://europepmc.org/articles/PMC8434274Test |
| حقوق: | OPEN |
| رقم الانضمام: | edsair.doi.dedup.....43281084ccc8b854546befe195da988f |
| قاعدة البيانات: | OpenAIRE |
| تدمد: | 19961944 |
|---|