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Real time color holographic interferometry devoted to 2D unsteady wake flows

机译:实时颜色全息干涉测量学专用于2D不稳定的唤醒流动

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A new optical technique based on real time holographic interferometry in trues colors has been implemented around the transonic wind tunnel of the ONERA-Lille center to analyze 2D unsteady wake flows. Tests realized in color interferometry, real time and double exposure, use simultaneously three wavelengths of a continuous waves laser (argon and krypton mixed) and holograms are recorded on silver-halide single-layer panchromatic Slavich PFG03c plates. The very principle of real-time true color holographic interferometry uses three primary wavelengths (red, green, blue) to record, under no-flow conditions, the interference among the three measurement beams and the three reference beams simultaneously on a single reference hologram. After the holographic plate is developed, it is placed on the test setup again in the position it occupied during exposure and the hologram is illuminated again by the three reference beams and three measurement beams. A flat, uniform color can then be observed behind the hologram. So a horizontal, vertical, or even circular fringe pattern can be formed and the achromatic central white fringe can be made out very clearly. This single color is used to determine the path difference zero on the interferograms. The flow studied was the unsteady flow downstream of a cylinder placed crosswise in the test section. A sequence of hundred interferograms was recorded on the flow around the cylinder at Mach 0.37. The vortex formation and dissipation phases can be seen very clearly, along with the fringe beat to either side of the cylinder.
机译:一种基于The Thrues Colors的实时全息干涉测量的新光学技术已经在Onera-Lille中心的跨音风隧道周围实施,分析了2D不稳定的唤醒流。在彩色干涉测量中实现的测试,实时和双曝光,同时使用连续波激光(氩气和氪混合)的三个波长,并在卤化银单层平面浆基PFG03C板上记录全息图。实时真正的颜色全息干涉测量法的原则是使用三个主波长(红色,绿色,蓝色)来在无流动条件下记录三个测量光束之间的干扰,以及在单个参考全息图上同时同时进行干扰。在开发全息板之后,在曝光期间占用的位置再次将其放置在测试设置上,并且通过三个参考光束和三个测量光束再次照亮全息图。然后可以在全息图后面观察到平坦的均匀颜色。因此,可以形成水平,垂直,甚至圆形条纹图案,并且可以非常清楚地制作化学中央白色边缘。这种单色用于确定干扰图上的路径差零。所研究的流程是在试验部分横向放置的气缸下游的不稳定流动。在Mach 0.37的气缸周围的流动上记录一百个干涉图。可以非常清楚地看到涡旋形成和耗散相,以及条纹敲打到气缸的任一侧。

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