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| 空天飞行器先进风洞实验技术及我国发展建议 | |
| 引用本文： | 吴根,姜宗林,罗凡. 空天飞行器先进风洞实验技术及我国发展建议[J]. 中国基础科学, 2014, 0(1): 13-16,12 |
| 作者姓名： | 吴根 姜宗林 罗凡 |
| 作者单位： | [1]科技部基础研究管理中心,北京100862 [2]高温气体动力学国家重点实验室（中国科学院力学研究所）,北京100190 |
| 摘 要： | 随着空间科学蓬勃发展，各国争相抢占空间科学的战略制高点，发展高超声速风洞技术的战略意义日渐凸显。我国在爆轰驱动高超声速激波风洞研究方面已经走在国际前列，核心技术具有自主知识产权。如何发挥已有设施的作用，加强风洞实验测量技术的研究与开发，提高实验数据的分析能力和在实际空天工程中的应用是我国下一步需要思考的问题。 |
| 关 键 词： | 高超声速风洞 爆轰驱动 发展建议 |
Advanced Wind Tunnel Testing Techniques of Aero- space Vehicle and Suggestions for Its Future De-velopment in China |
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| Wu Gen,Jiang Zonglin,Luo Fan. Advanced Wind Tunnel Testing Techniques of Aero- space Vehicle and Suggestions for Its Future De-velopment in China[J]. China Basic Science, 2014, 0(1): 13-16,12 | |
| Authors: | Wu Gen Jiang Zonglin Luo Fan |
| Affiliation: | 1. Department of Basic Research of Ministry of Science and Technology of People＇s Republic of China, Beijing 100862 ;2. State Key Laboratory of High-temperature Gas Dynamics, Institute of Mechanics, Chinese Academy of Sciences, Beijing 100190) |
| Abstract: | With the rapid development of space science and the intense competitions among countries for the strate-gic commanding height in this area , the strategic signifi-cance of developing hypersonic wind tunnel techniques is gradually becoming more and more obvious .China has become one of the front runners in the world in the research of detonation-driven hypervelocity shock tunnel and we possess Independent Intellectual property rights for our core technologies .Therefore, next,China should begin to consider how to fully utilize the existing facili-ties, strengthen the researches and development in shock tunnel testing measurement , and improve its ca-pabilities of analyzing experimental data and applying them into practical aerospace projects . |
| Keywords: | aerospace science detonation-driven shock tunnel development suggestion |
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