加热和冷却管道中可压缩单相流的参考解

S. Schropff, F. Petitpas, E. Daniel
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摘要

本文提出了在先加热后冷却的直线管道中稳定、可压缩、单相流动的分析/准分析解决方案。流动由上游水箱和可变出口压力之间的压力比驱动。文章提出了一种根据压力比和热流分布确定全流特性的方法。根据对喷嘴中可压缩流研究的类比,通过临界压力比的定义,提出了非绝热可压缩流的行为分类。研究表明,临界压力比可以区分亚音速和超音速出口状态,在这种配置下不可能存在稳定的冲击波。研究了这一临界压力比在热通量极限情况下的行为,划定了物理边界。还针对给定的加热功率和冷却功率提出了一个算盘,因为需要这两个值来描述流动的特征。对压力比和出口热功率等参数的结果进行了研究。对数值模拟工具进行了简短的验证,结果非常出色,相对误差非常小。
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Reference solutions for compressible single-phase flows in heated and cooled ducts
Analytical/quasi-analytical solutions are proposed for a steady, compressible, single-phase flow in a rectilinear duct subjected to heating followed by cooling. The flow is driven by the pressure ratio between an upstream tank and a variable outlet pressure. The article proposes a methodology to determine the full flow behavior, as a function of pressure ratio and heat-flux distribution. Following an analogy done with the study of compressible flows in nozzles, a behavioral classification of non-adiabatic compressible flows is proposed through the definition of critical pressure ratios. It is demonstrated that a critical pressure ratio distinguishes subsonic and supersonic outlet regimes and that there cannot be a steady shock wave in such configuration. The behavior of this critical pressure ratio is studied for limit cases of heat flux, delineating physical boundaries. An abacus is also proposed for a given couple of heating and cooling powers, as both values are needed to characterize the flow. Results are studied for parameters such as pressure ratio and outlet heat power. A short validation of a numerical simulation tool is provided, yielding excellent results and very small relative errors.
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