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Loss Analysis of Unsteady Turbomachinery Flows Based on the Mechanical Work Potential

机译:基于机械工作潜力的非稳态涡轮机流动的损耗分析

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Loss analysis is a valuable technique for improving the thermodynamic performance of tur-bomachines. Analyzing loss in terms of the "mechanical work potential" (Miller, R.J., ASME Turbo Expo 2013, GT2013-95488) provides an instantaneous and local account of the thermal and aerodynamic mechanisms contributing to the loss of thermodynamic performance. This study develops the practical application of mechanical work potential loss analysis, providing the mathematical formulations necessary to perform loss analysis using practical Reynolds-averaged Navier-Stokes (RANS) or large eddy simulations (LES). The analysis approach is demonstrated using RANS and LES of a linear compressor cascade, both with and without incoming wakes. Spatial segmentation is used to attribute loss contributions to specific regions of the flow, and phase-averaging is performed in order to associate the variation of different loss contributions with the periodic passage of wakes through the cascade. For this un-cooled linear cascade, viscous dissipation is the dominant source of loss. The analysis shows that the contribution of the viscous reheat effect depends on the operating pressure of the compressor stage relative to the ambient "dead state " pressure- implying that the optimal blade profile for a low-pressure compressor stage may be different from the optimal profile for a high-pressure compressor stage in the same engine, even if the operating conditions for both stages are dynamically similar.
机译:损失分析是一种有价值的技术,可提高突厥线的热力学性能。分析“机械工作潜力”(Miller,R.J.,Asme Turbo Expo 2013,GT2013-95488)的分析损失提供了导致热力和空气动力学机制的瞬时和本地叙述,导致热力学性能丧失。本研究开发了机械工作潜在损失分析的实际应用,提供了使用实用雷诺平均的Navier-Stokes(RAN)或大型涡流模拟(LES)进行损失分析所需的数学制片。使用RAN和LES的线性压缩机级联的rans和LES来证明分析方法,无论是在没有传入的唤醒。空间分割用于将损失贡献属于流程的特定区域,并且执行相位平均,以便将不同损耗贡献的变化与通过级联的周期性通道相关联。对于这种未冷却的线性级联,粘性耗散是主要的损失来源。分析表明,粘性再加热效果的贡献取决于压缩机级相对于环境“死态”的工作压力 - 暗示低压压缩机级的最佳刀片轮廓可以与最佳轮廓不同对于同一发动机中的高压压缩机级,即使两个阶段的操作条件是动态相似的。

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