Simultaneous spatially resolved temperature, pressure, and velocity measurements in high-enthalpy gas environments using spectrally resolved laser-induced fluorescence of potassium vapor
Joshua A. Vandervort, Spencer C. Barnes, Sean Clees, Christopher L. Strand, Ronald K. Hanson
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引用次数: 0
Abstract
A novel, absorption lineshape-based, laser-induced fluorescence diagnostic has been developed for simultaneous, single-point measurements of temperature, pressure, and velocity in high-enthalpy flow environments. The technique uses wavelength-tuned, narrow-linewidth, continuous-wave lasers to excite atomic potassium vapor, which is used as a flow tracer. The laser pumps the potassium D2 electronic transition, near 766.7 nm, while fluorescence from both the D1 and D2 lines is monitored simultaneously. The technique uses spectral lineshape and line position for inferring flow field properties, eliminating the need for detailed, setup-dependent calibration factors for quantitative measurements. The technique was tested and validated in argon and nitrogen in a shock tube with temperatures, pressures, and velocities ranging from 1000-2600 K, 0.1\(-\)0.7 atm, and 650-1200 m/s. Measurement volumes and uncertainties were as low as 3.5 \(\hbox {mm}^3\) and 5%, respectively, and measurement rates were up to 100 kHz. Accurate understanding of temperature, pressure, and velocity enables a more complete characterization of a compressible flow system as other quantities, including mass flux, Mach number, thrust, and stagnation conditions, can be calculated.
一种新型的、基于吸收线形的激光诱导荧光诊断技术已经被开发出来,用于在高焓流环境中同时、单点测量温度、压力和速度。该技术使用波长调谐,窄线宽,连续波激光来激发原子钾蒸气,它被用作流动示踪剂。激光泵浦D2钾在766.7 nm附近的电子跃迁,同时监测D1和D2线的荧光。该技术使用谱线形状和谱线位置来推断流场特性,从而消除了对定量测量的详细的、依赖于设置的校准因素的需要。该技术在激波管中氩气和氮气中进行了测试和验证,温度、压力和速度范围为1000-2600 K, 0.1 \(-\) 0.7 atm, 650-1200 m/s。测量体积和不确定度低至3.5 \(\hbox {mm}^3\)和5%, respectively, and measurement rates were up to 100 kHz. Accurate understanding of temperature, pressure, and velocity enables a more complete characterization of a compressible flow system as other quantities, including mass flux, Mach number, thrust, and stagnation conditions, can be calculated.
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