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Interaction between an upstream facing wall jet and a supersonic stream

机译:上游壁喷流与超音速流之间的相互作用

摘要

The flow field resulting from the interaction of an upstream facing wall jet with a supersonic counterflowing stream has been investigated. A flow field model and the main parameters governing the phenomena were determined from quantitative and qualitative experimental observations. Experimental results for different ranges of the main parameters are presented. A theoretical analysis was performed to describe the flow field in the mixing region between the two counterflowing streams. The results obtained by applying a locally similar solution compare favorably with the experimentally measured values. Large values of jet penetration were obtained with a high subsonic or low supersonic jet; large interaction forces are characteristics of higher supersonic injections. For the case of large penetration the cooling effectiveness presented as a function of the main parameters indicates the possibility of interacting cooling applications.
机译:已经研究了上游面壁射流与超音速逆流流相互作用产生的流场。流场模型和控制现象的主要参数是从定量和定性的实验观察中确定的。给出了主要参数不同范围的实验结果。进行了理论分析,以描述两个逆流之间的混合区域中的流场。通过应用局部相似的溶液获得的结果与实验测量值相比具有优势。高亚音速或低超音速射流可获得较大的射流穿透值;较大的相互作用力是较高超声速注入的特征。对于大穿透力的情况,作为主要参数的函数呈现的冷却效率表明了相互作用的冷却应用的可能性。

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  • 作者

    Piva R.;

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  • 年度 1972
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