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Application of Focused Laser Differential Interferometry (FLDI) in a Supersonic Boundary Layer

机译:聚焦激光微分干涉术(FLDI)在超音速边界层中的应用

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Single-point and two-point focused laser differential interferometry (FLDI) are used to explore the structure of a turbulent boundary layer in a Mach 2.6 in-draft wind tunnel's test section. Single point FLDI is used to measure density fluctuation profiles above the wall. Comparison of these profiles to Schlieren images is used to establish criteria for inferring boundary layer thickness from the FLDI measurements. Two-point FLDI can measure velocities of disturbances which pass through two FLDI measurement volumes. Within the bounds of uncertainty, velocity profiles measured using FLDI compare well to earlier measurements made using Pitot probes, Particle Image Velocimetry (PIV), and Krypton Tagging Velocimetry (KTV). Bandpass filtering the FLDI signal allows measurements of disturbance velocities at different frequencies. Higher frequency bands yield greater disturbance velocities than lower frequency bands in the investigated region of the boundary layer.
机译:单点和两点聚焦激光微分干涉法(FLDI)用于探索2.6马赫气流法风洞测试区中湍流边界层的结构。单点FLDI用于测量墙上方的密度波动曲线。这些轮廓与Schlieren图像的比较用于建立从FLDI测量中推断边界层厚度的标准。两点FLDI可以测量通过两个FLDI测量体积的干扰速度。在不确定性的范围内,使用FLDI测量的速度曲线与使用Pitot探针,粒子图像测速(PIV)和K标记测速(KTV)进行的较早的测量结果相当。带通滤波FLDI信号允许测量不同频率下的干扰速度。在边界层的研究区域中,较高的频段比较低的频段产生更大的干扰速度。

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