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Effect of strong refraction of probing beam accompanying shear holographic interferometry of a bow shock

机译:探测光束伴随剪切全息干涉测量的强折射的影响

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Preliminary results of optical diagnostics of bow shocks in a supersonic wind tunnel by applying dual-hologram shear interferometry technique are discussed. A strong refraction effect of the probing beam penetrating a region in the vicinity of a bow shock over a blunt nose cone model has been discovered. On a signal hologram the effect leads to the disappearance of holographic fringes in a narrow region attached to the shock wave front. A reconstructed interferogram in this region, being illuminated only by the comparison wave, manifests the absent of an interference pattern. Computer simulations were performed for a part of the probing beam penetrating the area of high-density steep-gradients of compressed air attaching to the central part of the shock front of a bow shock. The compressed area was modeled as a hyperbolic cap. The bow shock was assumed axisymmetric. The simulations made it possible to determine angles of deflections and found conformity with reconstructed interferograms (shadowgraph). It is concluded that in the above indicated region of bow shocks probing light is deviated refractively into some angles, which could be large enough for light rays to be blocked out and never arrive at detector (photo film). In the case, when interferometric fringes disappear the effect of strong refraction makes it impossible measuring of air density gradients in some critical region.
机译:探讨了通过施加双全息图剪切干涉技术,探讨了超声风隧道中弓形冲击光学诊断的初步结果。已经发现,已经发现了探测光束的强折射效果,其渗透在钝鼻锥模型上的凸起震动附近的区域。在信号全息图上,效果导致全息条纹在连接到冲击波前面的狭窄区域中的消失。该区域中的重建干涉图仅被比较波照射,表明了干扰图案的不存在。对探测光束的一部分进行计算机仿真,穿透压缩空气的高密度陡梯度的区域附接到蝶背震动的冲击前部的中心部分。压缩区域被建模为双曲线盖。轴对称凸起震动。模拟使得可以确定偏转角,并发现与重建的干扰图(ShadowGraph)确定符合性。得出结论,在上面所示的弓形冲击区域中,探测光被射击偏离成一定角度,这可能是足够大的,以便被封堵并从未到达检测器(摄影膜)。在这种情况下,当干涉仪消失时,强折射的效果使得在一些关键区域中不可能测量空气密度梯度。

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