高焓激波风洞有效试验时间标定研究

Study on calibration of effective test time in high enthalpy shock tunnel

  • 摘要: 为准确获得高压氢气驱动空气运行的激波风洞高焓流场有效试验时间,针对50 MPa氢气驱动0.1 MPa空气的激波风洞运行工况,分别采用高频压力传感器技术、高频热电偶技术、高频TDLAS的水组分测量技术,并结合CFD数值模拟,对激波风洞高焓运行过程及试验流场的有效试验时间进行了标定研究。结果表明:驱动段的高压氢气和被驱动段的空气在接触区域会发生燃烧,燃烧会导致激波管局部区域温度显著升高,燃烧产生的水会扩散到低压段的空气中,对试验气体造成污染,从而缩短激波风洞有效试验时间,高频热电偶球头驻点热流测量技术和基于TDLAS的水组分测量技术能够有效识别氢气/空气接触面到达时刻,实现激波风洞高焓流场有效试验时间的定量化测量,试验测得超高速空气动力研究所Φ2米激波风洞A在上述运行工况下,马赫数10流场的有效试验时间为2.6 ms。

     

    Abstract: In order to accurately obtain the effective experimental time of the high-enthalpy flow field in the shock wind tunnel driven by high-pressure hydrogen, the high-frequency pressure sensor technology, high-frequency thermocouple technology and high-frequency TDLAS water component measurement technology were used to calibrate the high enthalpy operation process and the effective test time of the test flow field in the shock tunnel with 50 MPa hydrogen driving 0.1 MPa air, combined with CFD numerical simulation. The results show that the high-pressure hydrogen gas in the driving section and the air in the driven section would burn in the contact area, causing a significant increase in temperature in the local area of the shock tube. The water produced by the combustion would diffuse into the air in the low-pressure section, causing pollution to the test gas and shortening the effective test time of the shock tunnel. The high-frequency heat flux measurement technology and the water component measurement technology based on TDLAS can effectively identify the arrival time of the hydrogen/air contact surface and realize the quantitative measurement of the effective test time of the high-enthalpy flow field in the shock tunnel. The effective test time of the Mach number 10 flow field in the Φ2 m shock tunnel A of the Hypervelocity Aerodynamics Institute under the above operating conditions is 2.6 milliseconds.

     

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