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NONSTATIONARY SHOCK REFLECTION OVER NONSTRAIGHT SURFACES - AN APPROACH WITH A METHOD OF MULTIPLE STEPS

机译:非直线表面上的非平稳冲击反射-一种采用多步法的方法

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Shock reflection phenomena over nonstraight surfaces have been investigated. The models used in this experiment are ordinary circular cylindrical concave and convex wedges and step-like wedges which simulate the former. The step-like wedges were used to investigate the process of reflected-wave formation over circular cylindrical wedges (method of multiple steps). The reflected-wave structure has been photographed with a schlieren apparatus. The formation of the reflected wave over circular cylindrical wedges is physically well understood by comparing it with shock reflection over step-like wedges. In particular, the reason why the reflected wave over a concave circular cylindrical wedge is very weak away from the reflection point is elucidated. Moreover, the structure and the formation mechanism of the so-called transitioned regular reflection (TRR) are illustrated in detail. As a by-product, based on acoustic theory, analytical formulae for the transition wedge angle are found. They are in good agreement with experiments. [References: 20]
机译:已经研究了非平直表面上的冲击反射现象。本实验中使用的模型是普通的圆柱凹凸楔和模拟前者的阶梯状楔。使用阶梯状的楔形物来研究在圆柱形楔形物上的反射波形成过程(多个步骤的方法)。反射波的结构已经用席利伦仪器拍摄了。通过将其与阶梯状楔形物上的冲击反射进行比较,可以很好地理解圆柱形楔形物上的反射波的形成。特别地,阐明了在凹形的圆柱形楔形物上的反射波远离反射点非常弱的原因。此外,详细示出了所谓的过渡正反射(TRR)的结构和形成机理。作为副产品,根据声学理论,可以找到过渡楔角的解析公式。他们与实验非常吻合。 [参考:20]

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