Turbulent mixing between a shock-accelerated vortex ring and its surroundings

冲击加速涡环与其周围环境之间的湍流混合

• 批准号: 1939809
• 负责人: Riccardo Bonazza
• 金额: $ 31.99万
• 依托单位: University of Wisconsin-Madison
• 依托单位国家: 美国
• 项目类别: Standard Grant
• 财政年份: 2020
• 资助国家: 美国
• 起止时间: 2020-01-15 至 2023-06-30
• 项目状态: 已结题
• 来源: https://www.nsf.gov/awardsearch/showAward?AWD_ID=1939809&HistoricalAwards=false
• 关键词: Turbulent; mixing; between; shock; accelerated

When a shock wave propagates through a region occupied by different gases, it generates gas motions at the wave boundary that lead to mixing at much higher rates than would have occurred in the absence of the shock wave. Phenomena of this kind can occur in a category of jet engines designed to operate at extremely high speeds that are much higher than those used in conventional jet transport. The study of these kinds of flows is generally very challenging because flow properties such as velocity, local gas composition, and temperature vary in space and time in very complicated ways. This research project will study a simple version of this type of flow. The researchers will study the response of a vortex ring to impulsive acceleration. By the nature of the vortex ring flow field, this initial condition should contain a much more coherent, well organized, predictable and measurable vorticity field than that of the jet engine. The results will form a highly refined building block database which could be used to develop a predictive capability for the more complicated version of these flows. Graduate and undergraduate students will be heavily involved in the research, with members of underrepresented minorities recruited through different programs already existing on campus. This project also will provide education in and exposure to state-of-the-art technologies and some of the most current challenges in science and engineering. The turbulent mixing induced by the interaction of a planar shock wave with a vortex ring consisting of a gas different than its surroundings will be investigated using planar laser induced fluorescence (PLIF) and particle image velocimetry (PIV). The goal of the project is to measure some of the most relevant flow properties, including the concentrations of the two gas species and their velocities everywhere within the region where the gases mix. This objective will be pursued in two different ways: 1) measurements will be made at discrete instants in time, with very high spatial resolution, and 2) measurements will be carried out with lesser spatial resolution but using an imaging system that will allow to collect entire concentration fields at a rate of up to 20,000 fields per second.This award reflects NSF's statutory mission and has been deemed worthy of support through evaluation using the Foundation's intellectual merit and broader impacts review criteria.

当冲击波传播通过不同气体占据的区域时，它会在波边界处产生气体运动，导致混合速度比没有冲击波时高得多。这种现象可能发生在设计用于以比传统喷气运输中使用的速度高得多的极高速度运行的喷气发动机中。对这类流动的研究通常非常具有挑战性，因为速度、局部气体成分和温度等流动特性在空间和时间上以非常复杂的方式变化。该研究项目将研究此类流程的简单版本。研究人员将研究涡环对脉冲加速度的响应。根据涡环流场的性质，该初始条件应包含比喷气发动机的涡度场更加连贯、组织良好、可预测和可测量的涡度场。结果将形成一个高度精炼的构建块数据库，可用于开发这些流程的更复杂版本的预测能力。研究生和本科生将大量参与这项研究，并通过校园现有的不同项目招募代表性不足的少数族裔成员。该项目还将提供最先进技术以及科学和工程领域当前一些挑战的教育和接触。将使用平面激光诱导荧光 (PLIF) 和粒子图像测速 (PIV) 研究由平面冲击波与由不同于周围环境的气体组成的涡环相互作用引起的湍流混合。该项目的目标是测量一些最相关的流动特性，包括两种气体的浓度及其在气体混合区域内各处的速度。该目标将以两种不同的方式实现：1) 测量将以非常高的空间分辨率在离散瞬间进行，2) 测量将以较低的空间分辨率进行，但使用的成像系统能够以每秒 20,000 个场的速率收集整个浓度场。该奖项反映了 NSF 的法定使命，并通过使用基金会的智力价值进行评估，被认为值得支持。 以及更广泛的影响审查标准。