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100-kHz PLEET for hypersonic flow velocity measurements in a Mach 6 Ludwieg Tube

机译:100 kHz PLEET用于在6马赫Ludwieg管中进行高超声速测量

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Picosecond-laser-electronic-excitation (PEET), a non-intrusive seedless velocimetry technique, is demonstrated in an AFRL Mach-6 Ludwieg tube at repetition rate of 100 kHz employing a 1064-nm, 100 ps, burst-mode laser. The system performance for high-speed velocimetry in unseeded air and nitrogen Mach-6 flows at a very-low static pressure range of 8-20 torr was evaluated. Time-resolved PLEET velocity measurements were performed in freestream and with a 14-degree cone model. Based on freestream flow measurement and computational fluid dynamics (CFD) calculation, we conclude that the measurement uncertainty of 100-kHz PLEET measurement for Mach 6 flow is less than 1%. The measured velocity profdes for model case also showed good agreement with CFD calculation before shock wave. Behind the Shockwave, the observed discrepancy between CFD and experimental measurement could attribute to the fluctuation of the cone model attacking angle during the experiment. Our results showed promise for utilizing 100-kHz PLEET velocimetry to understand real-time dynamics of turbulent hypersonic flows and provide capability to collect sufficient data in fewer test run in real hypersonic facilities.
机译:皮秒激光电子激发(PEET)是一种非侵入式无核测速技术,使用1064 nm,100 ps突发模式激光在AFRL Mach-6 Ludwieg管中以100 kHz的重复频率进行了演示。评估了在8-20托的非常低的静压范围内,在非播种的空气和氮气中的高速测速仪的系统性能,Mach-6流量。时间分辨的PLEET速度测量是在自由流中和14度锥模型中进行的。基于自由流流量测量和计算流体力学(CFD)计算,我们得出结论:对于6马赫流量,100 kHz PLEET测量的测量不确定度小于1%。模拟情况下测得的速度曲线也与冲击波前的CFD计算结果吻合良好。在冲击波后面,观察到的CFD与实验测量值之间的差异可能归因于实验过程中圆锥模型攻角的波动。我们的结果表明,利用100 kHz PLEET测速技术了解湍流高超音速流动的实时动态,并提供了在真正的高超音速设施中以较少的测试运行收集足够数据的能力。

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