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中文核心期刊

高速界面流动的激波管实验研究进展

ADVANCES IN SHOCK TUBE EXPERIMENTAL INVESTIGATION FOR HIGH-SPEED INTERFACIAL FLOWS

  • 摘要: 激波诱导流体界面不稳定性广泛存在于惯性约束核聚变、高超声速科技等重大工程中, 在涡动力学、流动稳定性、湍流形成机理等方面具有重要的科学意义. 相关研究的挑战性主要源于: 一方面, 激波作为传播速度大于声速的强间断扰动波, 其前后流场的速度、温度、压力等物理参数存在突变; 另一方面, 流体界面是流动复杂性的重要来源, 界面处的物理量间断显著加剧流动结构和形态的变化. 已有研究表明, 激波管在高速界面流动问题研究方面具有独特优势, 可以得到高时空分辨率的实验图像和可靠的基础数据. 基于此, 首先回顾了激波管中汇聚激波的可控生成原理与方法, 分别介绍了水平和竖直环形同轴激波管、半环形汇聚激波管、圆锥形汇聚激波管以及楔形汇聚激波管的设备结构和特点. 汇报了强激波诱导高速界面流动实验技术和流动机理方面的最新进展, 给出了激波管连续光滑弯曲管道壁面设计的理论方法和逆向设计思路, 实验验证了高强度激波管实验系统的稳定性、可靠性和可重复性, 并获得了激波传播过程中的完整波系演化与界面结构发展的时序数据, 阐明了激波接近效应和二次压缩效应等对扰动非线性演化的作用机制. 最后, 对高速界面流动实验研究面临的关键问题及其发展趋势进行了展望.

     

    Abstract: Shock-induced fluid interfacial instability has wide applications in some major projects such as inertial confinement fusion and hypersonic technologies, and has significant scientific significance in aspects such as vortex dynamics, flow stability, and the formation mechanism of turbulence. The challenges of the relevant problem mainly lie in two aspects. On one side, the shock waves, referred to as strong discontinuous disturbance waves with a propagation speed greater than the speed of sound, have sudden changes in physical parameters such as velocity, temperature and pressure in the flow fields before and after them. On the other side, the fluid interface is an important source of flow complexity, and the intermittent physical quantities at the interface significantly intensify the changes in the flow structure and morphology. Existing studies have shown that shock tubes have unique advantages in the research of high-speed interfacial flow problems, and can provide experimental images with high spatiotemporal resolution and reliable basic data. Here, the controllable generation principles and methods of converging shock waves in shock tubes were reviewed first. The equipment structures and characteristics of horizontal and vertical annular coaxial shock tubes, semi-annular converging shock tubes, conical converging shock tubes and wedge-shaped converging shock tubes were introduced, respectively. Furthermore, the latest progresses in the experimental techniques and flow mechanisms of high-speed interfacial flow induced by strong shock waves were reported. The theoretical methods and reverse design principles for the continuously smooth curved pipe wall design of shock tubes were presented. The stability, reliability and repeatability of the high-intensity shock tube experimental system were verified experimentally. The data of complete wave system evolution and interface structure development during the shock wave propagation process were obtained, and the mechanisms of shock proximity and secondary compression effects on the nonlinear evolution of disturbances were clarified. Finally, the key issues and development trends faced by the experimental research on high-speed interfacial flows were prospected.

     

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