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Coherent structures shed by multiscale cut-in trailing edge serrations on lifting wings

机译:多尺度切割后沿着翼翼锯齿的相干结构

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This experimental study presents the effect of multiscale cut-in trailing edge serrations on the coherent structures shed into the wake of a lifting wing. Two-probe span-wise hot-wire traverses are performed to study spectra, coherence, and phase shift. In addition, planar particle image velocimetry is used to study the spatio-temporal structure of the vortices shed by the airfoils. Compared with a single tone sinusoidal serration, the multiscale ones reduce the vortex shedding energy as well as the span-wise coherence. Results indicate that the vortex shedding is locked into an arch-shaped cell structure. This structure is weakened by the multiscale patterns, which explains the reduction in both shedding energy and coherence.
机译:该实验研究介绍了多尺度切割后边缘锯齿对沿升降翼尾的相干结构的效果。 进行双探针跨度热线遍历以研究光谱,相干性和相移。 另外,平面粒子图像速度测量法用于研究翼型旋流的涡流的时空结构。 与单音正弦锯齿相比,多尺度减少了涡旋脱落能量以及跨度明智的相干性。 结果表明涡旋脱落被锁定成拱形电池结构。 这种结构被多尺度模式削弱,这解释了脱落能量和连贯性的减少。

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