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Aperture Effects on Aero-Optical Distortions Caused by Subsonic Boundary Layers

机译:亚音区边界层引起的空气光学扭曲的光圈效应

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Results of experimental measurements of aero-optical distortions caused by turbulent boundary layers at subsonic speeds M = 0.4...0.6 are presented. Measurements were performed using a high-speed Shack-Hartmann sensor and a Malley probe to collect instantaneous wavefronts with high spatial and temporal resolution. Effects of different aperture sizes on levels of aero-optical aberrations and correlation lengths in both spanwise and streamwise directions are compared and discussed for both wavefront sensors. Detailed statistical analysis of spatial and temporal spectra of aero-optical distortions is presented. Analytical method to predict levels of aero-optical distortions and streamwise correlation lengths for different aperture sizes is proposed and it was found to agree with experimental results. The contribution of boundary-layer large- and small-scale structures on overall level of aero-optical distortions is examined and discussed.
机译:提出了由余弦速度下湍流边界层引起的气相 - 光学扭曲的实验测量结果M = 0.4 ... 0.6。使用高速Shack-Hartmann传感器和麦利探头进行测量,以收集具有高空间和时间分辨率的瞬时波前。比较和讨论不同孔径尺寸对空气 - 光学像差水平的影响,并讨论了两条波前传感器。介绍了航空光学扭曲的空间和时间光谱的详细统计分析。提出了预测不同孔径尺寸的航空失真水平和流动相关长度的分析方法,发现它与实验结果一致。检查并讨论了边界层大型和小规模结构对整体水平的整体水平的贡献。

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