Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon | |
Jiang ZL(姜宗林)![]() ![]() | |
Source Publication | 31st International Symposium on Shock Waves 1 |
2019-03-22 | |
Pages | 1-10 |
Conference Name | 31st International Symposium on Shock Waves |
Conference Date | 2017-07-9~14 |
Conference Place | Nagoya, Japan |
Abstract | In this paper, aerodynamic testing carried out with the JF12 hypervelocity shock tunnel is reported, and three experiments are discussed. The first experiment is aerodynamic heat test in hypersonic boundary layer, and a new thermal sensor for heat flux measurement at the extreme high-temperature condition is described, and the hypersonic boundary physics is explored. The second one is the aerodynamic force testing, and a new concept is proposed for optimizing the force and moment measurement system in shock tunnels. With this technology, the real gas effect is investigated, and its dominating mechanism is considered to be the gas molecular vibration. The last is the scramjet test from which two engine operation models are observed, that is, the continuous and pulsed combustion. Because most of the scramjet tests were conducted in combustion-based test facilities, the experimental data at the duplicated hypersonic flight condition would be of fundamental importance for exploring coupling of combustion, supersonic flow, and shock dynamics. |
ISBN | 978-3-319-91017-8 |
Language | 英语 |
Document Type | 会议论文 |
Identifier | http://dspace.imech.ac.cn/handle/311007/80806 |
Collection | 高温气体动力学国家重点实验室 |
Recommended Citation GB/T 7714 | Jiang ZL,Yu HR. Aerodynamic Testing at Duplicating Hypersonic Flight Conditions with Hyper-Dragon[C]31st International Symposium on Shock Waves 1,2019:1-10. |
Files in This Item: | Download All | |||||
File Name/Size | DocType | Version | Access | License | ||
Cp2019057.pdf(523KB) | 会议论文 | 开放获取 | CC BY-NC-SA | View Download |
Items in the repository are protected by copyright, with all rights reserved, unless otherwise indicated.
Edit Comment