Aerodynamic measurement of a large aircraft model in hypersonic flow | |
Meng BQ(孟宝清); Han GL(韩桂来); Zhang DL(张德良); Jiang ZL(姜宗林) | |
发表期刊 | CHINESE PHYSICS B |
2017-11-01 | |
卷号 | 26期号:11页码:114702-1-114702-6 |
ISSN | 1674-1056 |
摘要 | Accurate aerodynamic measurements in the hypersonic flow of large aircraft models in tunnels have practical significance, but pose a significant challenge. Novel aerodynamic force measurement methods have been proposed, but lack theoretical support. The forms of the force signals techniques for signal processing and calculation of aerodynamics are especially problematic. A theoretical study is conducted to investigate the dynamic properties based on models of the draw-rod system and slender rods. The results indicate that the inertia item can be neglected in the rod governing equation; further, the solutions show that the signals of each rod are a combination of aerodynamic signals (with a constant value) and sine signals, which can be verified by experimental shock tunnel results. Signal processing and aerodynamics calculation techniques are also found to be achievable via the flat part of the signals. |
关键词 | Hypersonic Aerodynamic Measurement Theoretical Study Vibration |
DOI | 10.1088/1674-1056/26/11/114702 |
收录类别 | SCI ; EI ; CSCD |
语种 | 英语 |
WOS记录号 | WOS:000415073400002 |
WOS研究方向 | Physics |
WOS类目 | Physics, Multidisciplinary |
项目资助者 | National Natural Science Foundation of China(11472281 ; 11532014) |
CSCD记录号 | CSCD:6125787 |
课题组名称 | LHD激波与爆轰物理 |
论文分区 | Q3 |
力学所作者排名 | 1 |
引用统计 | |
文献类型 | 期刊论文 |
条目标识符 | http://dspace.imech.ac.cn/handle/311007/71946 |
专题 | 高温气体动力学国家重点实验室 |
通讯作者 | Han GL(韩桂来) |
推荐引用方式 GB/T 7714 | Meng BQ,Han GL,Zhang DL,et al. Aerodynamic measurement of a large aircraft model in hypersonic flow[J]. CHINESE PHYSICS B,2017,26,11,:114702-1-114702-6. |
APA | Meng BQ,Han GL,Zhang DL,&Jiang ZL.(2017).Aerodynamic measurement of a large aircraft model in hypersonic flow.CHINESE PHYSICS B,26(11),114702-1-114702-6. |
MLA | Meng BQ,et al."Aerodynamic measurement of a large aircraft model in hypersonic flow".CHINESE PHYSICS B 26.11(2017):114702-1-114702-6. |
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