首页> 外文会议>AES-vol.45; ASME(American Society of Mechanical Engineers) International Mechanical Engineering Congress and Exposition; 20051105-11; Orlando,FL(US) >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程序的熵产生率: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)=∫_(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 ∫_(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。段落中的全局熵产生速率(dS)/(dt)=∫_(V(x,y,z))(ds)/(dt)dxdydz当然与级联效率直接相关,但是其依赖于流场局部特征的函数依赖关系无法立即检测到:左侧是单值量,因此不能用作逆向设计过程的目标函数(因为单个变量的局部修改)叶片几何形状的细节总是对整个流域产生不可忽略的影响。相反,了解通道每个点的局部熵生成率可立即了解过程中不可逆性不同来源的相对重要性。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,并且本质上是非系统的方法。另一方面,从理论和实践的角度来看,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∫_的叶片轮廓优化的示例。 (V(x,y,z))(ds)/(dt)dxdydz,要在设计域V上最小化。本文提出了局部和全局熵生成与模型的局部特征之间关系的合理推导。流程,并通过两个示例来说明它们,这些示例是由罗马大学1的作者领导的涡轮机械小组在最近几年开发的应用程序衍生的。使用这种“本地”方法的优缺点受到了严格的讨论。 ,并在结论中提出了一种程序,用于开发基于(ds)/(dt)的适当约束目标函数的逆设计方法:尽管从计算的角度来看非常密集,但有迹象表明在不久的将来,这种方法在现实的几何形状上可能变得可行。

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