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Integral density measurements in wing wake at Mach 2

机译:Mach 2的机翼唤醒中的积分密度测量

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Wind tunnel experiments often includes optical diagnostic of the flow. It is mostly used only for obtaining qualitative information on flow structure. However, interference methods also can provide quantitative information on density variations along the optical path length. A change in density of studied flow inhomogeneities leads to shift of fringes in the interference pattern. The results of the application of the optical method for determining the integral density field during the study of a vortex wing wake are presented. The optical diagnostics of the flow was performed by means of adaptive visualizing transparencies based on the saturation of absorption effect. To translate infinite interference fringes into finite ones, an optical wedge was used. The principal possibility of using the method for obtaining quantitative data on flow parameters in the study of the longitudinal end vortex is shown.
机译:风洞实验通常包括流量的光学诊断。它主要用于获得有关流动结构的定性信息。然而,干扰方法还可以提供关于沿光路长度的密度变化的定量信息。研究流动不均匀性密度的变化导致干涉图案中的条纹的偏移。介绍了在涡旋翼尾苏术研究期间确定积分密度场的光学方法的应用。通过基于吸收效应的饱和度,通过自适应可视化透明胶片进行流的光学诊断。将无限的干涉条纹转化为有限的干扰物,使用光学楔形物。示出了使用该方法获得关于纵向涡流的研究中获得定量数据方法的方法的主要可能性。

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