A Review of Multiphysics Coupling Mechanical Behavior of Titanium-Coated Heterogeneous Wing for Re-entry Hypersonic Vehicle
文献类型:期刊论文
作者 | Liu F(刘飞)5![]() ![]() ![]() |
刊名 | JOM
![]() |
出版日期 | 2024-09-18 |
页码 | 11 |
ISSN号 | 1047-4838 |
DOI | 10.1007/s11837-024-06878-8 |
通讯作者 | Huan, Yong(huany@lnm.imech.ac.cn) |
英文摘要 | The titanium-coated alloy heterogeneous structure has been widely used in the manufacture of re-entry hypersonic vehicle wings. However, due to the extreme and complex hypersonic service environment, the strength of the Ti alloy matrix is easily reduced under the synergistic action of complex loads such as aerodynamic heat, vibration, corrosion, and noise. This results in a mismatch of structural strength at the interface structure in the titanium-coated alloy, leading to destruction of the wing aerodynamic shape. At the same time, multiple load synergies can also lead to defects such as cracks and holes in the surface coating, damaging wing structural integrity. In addition, under the combined action of frequency- and time-domain loads, the wing structure will also experience creep deformation, leading to fatigue-creep interaction, exacerbating the accumulation of wing damage, and posing a serious threat to the service safety of the re-entry hypersonic vehicle. Therefore, this paper first reviews current research hotspots of re-entry hypersonic vehicle technology, and then analyzes the strengthening-toughening mechanism, high-temperature fatigue behavior, high-temperature creep behavior, and the damage prediction model of the titanium-coated alloy's heterogeneous structure. Finally, it summarizes and prospects future research directions. |
分类号 | 二类 |
WOS关键词 | FATIGUE BEHAVIOR ; CREEP-BEHAVIOR ; ALLOY ; OPTIMIZATION ; SIMULATION ; COMPOSITE ; DAMAGE |
资助项目 | National Natural Science Foundation of China[11972037] ; National Natural Science Foundation of China |
WOS研究方向 | Materials Science ; Metallurgy & Metallurgical Engineering ; Mineralogy ; Mining & Mineral Processing |
语种 | 英语 |
WOS记录号 | WOS:001315601200002 |
资助机构 | National Natural Science Foundation of China ; National Natural Science Foundation of China |
其他责任者 | Huan, Yong |
源URL | [http://dspace.imech.ac.cn/handle/311007/96715] ![]() |
专题 | 力学研究所_非线性力学国家重点实验室 |
作者单位 | 1.Univ Chinese Acad Sci, Sch Engn Sci, Beijing 100049, Peoples R China 2.Inner Mongolia Inst Met Mat, Baotou 014034, Peoples R China; 3.Xian Aerosp Engine Co Ltd, Xian 710100, Peoples R China; 4.AECC Hunan Aviat Powerplant Res Inst, Zhuzhou 412002, Peoples R China; 5.Chinese Acad Sci, State Key Lab Nonlinear Mech LNM, Inst Mech, Beijing 100190, Peoples R China; |
推荐引用方式 GB/T 7714 | Liu F,Li, Jiaqiang,Chen, Kunyu,et al. A Review of Multiphysics Coupling Mechanical Behavior of Titanium-Coated Heterogeneous Wing for Re-entry Hypersonic Vehicle[J]. JOM,2024:11. |
APA | 刘飞.,Li, Jiaqiang.,Chen, Kunyu.,Li, Yang.,Zhang, Mingyi.,...&郇勇.(2024).A Review of Multiphysics Coupling Mechanical Behavior of Titanium-Coated Heterogeneous Wing for Re-entry Hypersonic Vehicle.JOM,11. |
MLA | 刘飞,et al."A Review of Multiphysics Coupling Mechanical Behavior of Titanium-Coated Heterogeneous Wing for Re-entry Hypersonic Vehicle".JOM (2024):11. |
入库方式: OAI收割
来源:力学研究所
浏览0
下载0
收藏0
其他版本
除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。