有机蒸汽通过涡轮叶栅流动的临界和窒息马赫数

S. Wiesche, Felix Reinker, R. Wagner, L. Hake, Maximilian Passmann
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引用次数: 3

摘要

本文介绍了有机蒸汽通过涡轮叶栅的临界马赫数和窒息马赫数的理论和实验研究结果。利用对接近于单位的等熵指数有效的渐近级数展开,推导了预测有机蒸汽流动窒息马赫数的相关性。在闭环有机蒸汽风洞中,采用线性涡轮叶栅和圆柱对理论预测进行了验证。叶栅是基于经典的跨音速涡轮翼型,完美的气体文献数据是可用的。该叶栅采用选择性激光熔化(SLM)制造,并通过随后的表面处理建立了相当低的表面粗糙度水平。由于闭环风洞返回处安装了独立的质量流量传感器,且测试设施能够实现稳定的长期运行行为,因此可以高精度地获得阻塞马赫数。观察到非完美气体动力学会局部影响临界马赫数,但观察到的涡轮叶栅窒息行为与所考虑的稀释气体流型的渐近结果很好地吻合。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Critical and Choking Mach Numbers for Organic Vapor Flows Through Turbine Cascades
Results are presented of a theoretical and experimental study dealing with critical and choking Mach numbers of organic vapor flows through turbine cascades. A correlation was derived for predicting choking Mach numbers for organic vapor flows using an asymptotic series expansion valid for isentropic exponents close to unity. The theoretical prediction was tested employing a linear turbine cascade and a circular cylinder in a closed-loop organic vapor wind tunnel. The cascade was based on a classical transonic turbine airfoil for which perfect gas literature data were available. The cascade was manufactured by Selective Laser Melting (SLM), and a comparable low surface roughness level was established by subsequent surface finishing. Because the return of the closed-loop wind tunnel was equipped with an independent mass flow sensor and the test facility enabled stable long-term operation behavior, it was possible to obtain the choking Mach number with high accuracy. It was observed that non-perfect gas dynamics affect the critical Mach number locally, but the observed choking behavior of the turbine cascade was in good agreement with the asymptotic result for the considered dilute gas flow regime.
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