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Development of a tunable diode laser probe for measurements in hypervelocity flows.

机译:开发用于超高速流量测量的可调二极管激光探头。

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摘要

This thesis describes the development and demonstration of tunable-diode laser absorption spectroscopy (TDLAS) probes for ground-based hypervelocity flowfield measurements. Flight testing of hypervelocity systems exacts high risks and costs, thereby requiring ground-based testing in facilities such as reflected shock tunnels and shock/expansion tunnels. Diagnostics deployed in ground-based facilities measure pertinent performance parameters for flight-system evaluation. Therefore, an accurate assessment of the freestream thermodynamic-state is required for worthwhile data interpretation and CFD model validation.; The tunable diode-laser absorption technique's quantum and species-specific nature leads to direct flowfield measurements of velocity, temperature and target-species concentration. The probes are fiber-coupled to spectrally tuning lasers (at kilohertz rates) across tracer-absorption transitions. The probe pitches and catches laser beams that non-intrusively interrogate the flowfield. Analysis of the recorded laser-transmitted intensities from each scan yields parameter time-histories.; During gas-driven reflected shock tunnel operation, driver gas permeates the test gas. When testing in air with a hydrogen driver, the resultant water is exploited as a spectroscopic target. Temperature, concentration, and velocity are obtained from water absorption (near 1.4 mum). The measurements agreed well with the computationally predicted values of velocity and temperature (4500 m/s and 600 K). However, later in each test an increase in water vapor concentration correlated with a velocity increase and a varying temperature. In a separate study, a miniaturized probe was developed to measure velocity while targeting naturally present chemically-frozen, freestream potassium (near 0.77 mum). Velocity measurements were consistent with facility models and simultaneous water-vapor measurements.; Another miniature probe was developed to measure velocity at 30.3 kHz rates in shock/expansion tubes with water-seeded nitrogen. The average of the velocity measurements agreed well with traditional time-of-flight measurements. However, an initial unsteadiness, believed to be caused by facility boundary layer growth and/or the presence of a reflected shock, was observed.; This work successfully demonstrates that TDLAS probes are capable of making repeatable measurements in hypervelocity flowfields. Their value is highlighted by their ability to directly measure the flow composition time-history and thermodynamic state in high-enthalpy, ground-based flow facilities.
机译:本文描述了用于地面超高速流场测量的可调谐二极管激光吸收光谱(TDLAS)探头的开发和演示。超高速系统的飞行测试具有很高的风险和成本,因此需要在设施中进行地面测试,例如反射式冲击隧道和冲击/扩展隧道。部署在地面设施中的诊断程序会测量相关性能参数,以进行飞行系统评估。因此,需要对自由流热力学状态进行准确评估,以进行有价值的数据解释和CFD模型验证。可调二极管-激光吸收技术的量子和物种特定性质可导致对速度,温度和目标物种浓度进行直接流场测量。探针通过光纤耦合到在示踪剂吸收跃迁处的光谱调谐激光器(以千赫兹速率)。探头可俯仰并捕获激光束,该激光束不会侵入流场。从每次扫描中记录的激光透射强度的分析产生参数时间历史。在气体驱动的反射式冲击隧道操作中,驱动气体会渗透到测试气体中。使用氢气驱动器在空气中进行测试时,生成的水被用作光谱目标。温度,浓度和速度是通过吸水(接近1.4毫米)获得的。测量结果与速度和温度的计算预测值(4500 m / s和600 K)非常吻合。但是,稍后在每个测试中,水蒸气浓度的增加与速度增加和温度变化相关。在另一项研究中,开发了一种微型探针来测量速度,同时靶向天然存在的化学冷冻的自由流钾(0.77毫米附近)。速度测量值与设施模型和同时进行的水蒸气测量值一致。开发了另一款微型探头,用于在装有水晶氮的冲击/膨胀管中以30.3 kHz的速率测量速度。速度测量值的平均值与传统飞行时间测量值非常吻合。但是,观察到最初的不稳定,据认为是由设施边界层的增长和/或反射冲击的存在引起的。这项工作成功地证明了TDLAS探针能够在超高速流场中进行重复测量。它们的价值在于其能够直接测量高焓地面流动设施中的流动成分时间历史和热力学状态的能力。

著录项

  • 作者

    Wehe, Shawn David.;

  • 作者单位

    Stanford University.;

  • 授予单位 Stanford University.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2000
  • 页码 173 p.
  • 总页数 173
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类 机械、仪表工业;
  • 关键词

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