| 引用本文: | 周勇为,易仕和,程忠宇.Φ200高超声速风洞调试和流场校测.[J].国防科技大学学报,2009,31(6):57-61.[点击复制] |
| ZHOU Yongwei,YI Shihe,CHENG Zhongyu.The Test and Calibration of Φ200 Hypersonic Wind Tunnel[J].Journal of National University of Defense Technology,2009,31(6):57-61[点击复制] |
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| Φ200高超声速风洞调试和流场校测 |
| 周勇为, 易仕和, 程忠宇 |
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(国防科技大学 航天与材料工程学院，湖南 长沙 410073)
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| 摘要: |
| 介绍了新近建成的马赫数为2.5～7.0的Φ200mm高超声速风洞(Φ200 Hypersonic Wind Tunnel，HWT-200)调试情况及空风洞流场校测结果。调试校测结果表明，风洞的总温、总压、运行时间等参数完全达到了设计要求，顺利实现了宽马赫数范围下的超声速/高超声速运行；本风洞有较大的实验段流场均匀区，各流场的马赫数均方根偏差全部达到GJB(1179-91)的合格指标，一部分达到了先进指标。风洞运行时间不少于20s，是一座参数范围较宽、运行成本较低、维护方便、可用于空气动力学教学试验和基础性科学研究的设备。 |
| 关键词: 高超声速 风洞 风洞调试 流场校测 |
| DOI： |
| 投稿日期：2009-09-07 |
| 基金项目:国家部委资助项目 |
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| The Test and Calibration of Φ200 Hypersonic Wind Tunnel |
| ZHOU Yongwei, YI Shihe, CHENG Zhongyu |
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(College of Aerospace and Materials Engineering, National Univ. of Defense Technology, Changsha 410073, China)
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| Abstract: |
| The newly finished Φ200 hypersonic wind tunnel(Mach numbers 2.5 to 7) has been tested and calibrated. The results of calibration indicating total temperature, total pressure, operating time of HWT-200 have accorded with the purpose of design. HWT-200 can run within large Mach number span at supersonic/hypersonic flow. The rms of Mach numbers (σM) at all test sections Mach numbers from 2.5 to 7.0 reaches the requirement of GJB1179-91. A large, uniform region of flow was documented. Operational time of HWT-200 is no less than 20s. So, HWT-200 is a facility which can be used for teaching of aerodynamic experiments and elementary scientific researches. |
| Keywords: hypersonic wind tunnels test of wind tunnel calibration of flow field |
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