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首页> 外文期刊>Proceedings of the ASME Advanced Energy Systems Division >COMPUTING THE ENTROPY GENERATION RATE FOR TURBOMACHINERY DESIGN APPLICATIONS: CAN A DIAGNOSTIC TOOL BECOME A PREDICTIVE ONE?
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COMPUTING THE ENTROPY GENERATION RATE FOR TURBOMACHINERY DESIGN APPLICATIONS: CAN A DIAGNOSTIC TOOL BECOME A PREDICTIVE ONE?

机译:计算涡轮机械设计应用的熵产生率:诊断工具可以成为预测工具吗?

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The calculation of the entropy generation rate ds/dt in turbomachinery passages is a straightforward task once the velocity and temperature fields are known. The global entropy generation rate in the passage, dS/dt velence integral_(V(x,y,z)) ds/dt dxdydz, is of course directly related to the cascade efficiency, but its functional dependence on the local characteristics of the flowfield is not immediately detectable: the left-hand side is a single-valued quantity that cannot, as such, be used as the objective function of an inverse design procedure (because a local modification of a single detail of the blade geometry invariably produces non-negligible effects on the entire flow domain). On the contrary, knowledge of the local entropy generation rate in each point of a channel provides immediate useful insight into the relative importance of the different sources of irreversibility in the process. There are numerous examples of the application of entropy generation maps as a diagnostic design tool, i.e., to locate problematic areas that demand for design "improvements": these are, though, basically heuristic and intrinsically non-systematic approaches. On the other hand, the adoption of a functional based on the local entropy generation rates is difficult both from a theoretical and from a practical point of view, and there is no example yet of a blade profile optimization in which the objective function is integral_(V(x,y,z)) ds/dt dxdydz, to be minimized over the design domain V. This paper presents a rational derivation of the relationships between the local and global entropy generation and the local features of the flow, and illustrates them by means of two examples derived from applications developed in the last years by the Turbomachinery Group led by the author at the University of Roma 1. The merits and limits of the use of such a "local" approach are critically discussed, and in the Conclusions a procedure is proposed for the development of an inverse design approach based on a properly constrained objective function based on ds/dt: though quite intensive from a computational point of view, there are indications that such an approach may become feasible on realistic geometries in the near future.
机译:一旦知道速度和温度场,涡轮机械通道中的熵产生率ds / dt的计算就很简单。通道中的整体熵产生速率dS / dt velvel积分_(V(x,y,z))ds / dt dxdydz当然与级联效率直接相关,但其功能依赖于流场的局部特征不能立即检测到:左侧是单值量,因此不能用作逆设计程序的目标函数(因为局部修改叶片几何形状的单个细节总是会产生非对整个流域的影响可忽略不计)。相反,了解通道每个点的局部熵生成速率可立即了解过程中不同不可逆源的相对重要性。熵生成图作为诊断设计工具的应用有很多例子,例如,定位需要设计“改进”的问题区域:尽管这些基本上是启发式的,本质上是非系统的方法。另一方面,无论从理论上还是从实践的角度来看,都难以采用基于局部熵产生率的函数,并且还没有目标函数为integral _(( V(x,y,z))ds / dt dxdydz,要在设计域V上最小化。本文介绍了局部和全局熵生成与流的局部特征之间关系的合理推导,并对其进行了说明。通过两个例子,这些例子是由罗马大学1的作者领导的Turbomachinery小组在最近几年开发的应用程序得出的。对使用这种“本地”方法的优缺点进行了严格的讨论,在结论中提出了一种基于ds / dt的,基于适当约束的目标函数的逆设计方法的开发过程:尽管从计算的角度来看,这是相当繁琐的,但有迹象表明,在不久的将来,n方法可能会在实际几何形状上变得可行。

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