| 增设收缩截面后的爆轰驱动激波管性能研究 |
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| 引用本文： | 赵伟,姜宗林,王超.增设收缩截面后的爆轰驱动激波管性能研究[J].实验流体力学,2001,15(2):34-40. |
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| 作者姓名： | 赵伟 姜宗林 王超 |
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| 作者单位： | 中国科学院力学研究所LHD开放实验室, |
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| 基金项目： | Investigation on
Experimental Method of Developing Detonation Driver to Produce High Reynolds Test Flow |
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| 摘 要： | 为提高前向爆轰驱动激波风洞的性能，采用在驱动段靠近主膜处增设一个收缩喉道的方法，以此来产生较为均匀的驱动气源。实验结果表明此方法有效地削弱了爆轰波后Taylor稀疏波的影响。
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| 关 键 词： | 爆轰 爆轰驱动 激波 激波管 喉道 |
| 文章编号： | 1007-3124(02)-0034-07 |
| 修稿时间： | 2000年12月18 |
Performance of the
detonation driven shock tube with a converging throat |
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| ZHAO Wei,JIANG Zong-lin,WANG Chao.Performance of the
detonation driven shock tube with a converging throat[J].Experiments and Measur in Fluid Mechanics,2001,15(2):34-40. |
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| Authors: | ZHAO Wei JIANG Zong-lin WANG Chao |
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| Abstract: | In order to increase the performance of the detonation driven shock tunnel, some converging throats are added in driver section near the main diaphragm.Experimental results indicate that this way can availably weaken the effect of Taylor rarefaction waves. |
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| Keywords: | detonation detonation driver shock wave shock tube throat |
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