| 激波过弯道绕流流场(英文) |
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| 引用本文： | 叶希超,杨辉,乐嘉陵.激波过弯道绕流流场(英文)[J].实验流体力学,1997(1). |
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| 作者姓名： | 叶希超 杨辉 乐嘉陵 |
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| 作者单位： | 中国空气动力研究与发展中心!绵阳，621000，中国空气动力研究与发展中心!绵阳，621000，中国空气动力研究与发展中心!绵阳，621000 |
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| 摘 要： | 为了研究微波过弯道的传播，气动中心设计了微波过弯道的实验装置，它很容易拆卸并组成带10°发散的弯道、短形弯道和带各种角度的二元喷嘴。实验所得到的若干照片，对于研究激波反射、绕射与边界的相互作用和对数值模拟的验证是很有用的。
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| 关 键 词： | 激波 弯道 光栅干涉 超音速流动 实验结果 |
FLOW FIELD OF SHOCK WAVE THROUGH CURVED CHANNEL |
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| Ye Xichao,Yang Hui, Le Jialing.FLOW FIELD OF SHOCK WAVE THROUGH CURVED CHANNEL[J].Experiments and Measur in Fluid Mechanics,1997(1). |
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| Authors: | Ye Xichao Yang Hui Le Jialing |
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| Institution: | China Aerodynamics Research &. Development Center.Mianyang 621000 |
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| Abstract: | In order to investigate the shock wave propogation through curved channel, the experiment set of shock motion through curved channels has been designed at Facility Design & Instrumentation Institute of CARDC. It can be dismantled easily and constructed curved channel with a divergence of 10 degrees,rectangular curved channel and dual jet with various degrees,etc. The photos of shock wave have been obtained, These photos are usefulfor researching into shock reflection,diffraction and their interaction with boundary and affirming numerical simulation |
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| Keywords: | shock wave curved channel grating interference experimental result supersonic flow |
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