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EVALUATING COMPLEX INLET DISTORTION WITH A PARALLEL COMPRESSOR MODEL:PART 1 - CONCEPTS, THEORY, EXTENSIONS, AND LIMITATIONS

机译:用平行压缩机模型评估复杂的进气道变形:第一部分-概念,理论,扩展和局限性

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Modeling compression systems using parallel compressor theory has been used for the analysis of compression system operability since the 1960s. Parallel compressor models have been traditionally designed and used for the analysis of circumferential distortion effects as a means to evaluate the impact of various inlet flow field disturbances on compressor operation.This paper (the first of two) provides a review of the parallel compressor concept and discusses extensions to the original theory. These extensions include the incorporation of dynamic response, application to complex distortions, and the application to inlet swirl. Understanding these effects and the application of parallel compressor theory extensions is required to produce analytical models and computer simulations that can be used to enhance the development testing and the understanding of the response of gas turbine compression systems. Once a computer simulation has been constructed for a particular test article, it can be exercised and results compared against test results where distortion-generator devices (such as distortion screens) have been used, generally with favorable accuracy. The usefulness of the extended parallel compressor model is derived from its ease of use, simplicity, and ability for quick turn-around of results. It is often more desirable to have an analysis capability that is easy and quick to use than to have one that is extremely accurate, especially when understanding basic physics is of primary concern during a test operation. Extreme accuracy may require large amounts of computer resources and take days or weeks to compute a single performance point. While this may be acceptable for design, the limitations of high-fidelity simulations make them impractical to use due to the time constraints imposed by the pace of testing. Applying a timely analysis capability, using a par-allel compressor simulation can provide a new physical understanding of the effects of complex distortion during the testing process when comparing the analytical and test results. This concept is presented in two companion papers: the first paper, Part 1, concentrates on the parallel compressor concepts, theory and limitations of the methodology while the second paper, Part 2 [1] presents applications of the approximate methods developed and compares results with experimental data.
机译:自1960年代以来,就一直使用并行压缩机理论对压缩系统进行建模,以分析压缩系统的可操作性。传统上设计了并联压缩机模型,并将其用于分析周向畸变效应,以评估各种入口流场干扰对压缩机运行的影响。讨论对原始理论的扩展。这些扩展包括动态响应的合并,复杂失真的应用以及进气涡流的应用。需要了解这些影响以及并行压缩机理论扩展的应用,才能生成可用于增强开发测试和对燃气轮机压缩系统响应的理解的分析模型和计算机模拟。一旦为特定的测试项目构建了计算机模拟,就可以对其进行练习,并将结果与​​使用失真发生器设备(例如失真屏幕)的测试结果进行比较(通常具有良好的准确性)。扩展的并行压缩器模型的实用性源于其易用性,简单性以及快速转换结果的能力。通常,更需要一种易于使用且快速的分析功能,而不是具有极其准确的分析功能,尤其是在测试操作过程中最先要了解基本物理原理的情况下。极高的准确性可能需要大量的计算机资源,并且要花费数天或数周的时间才能计算出单个性能点。尽管这对于设计来说是可以接受的,但是由于测试步伐带来的时间限制,高保真模拟的局限性使其无法使用。在比较分析结果和测试结果时,应用及时分析功能,使用并行压缩器仿真可以对测试过程中复杂失真的影响提供新的物理理解。该概念在两篇随附的论文中得到介绍:第一篇论文,第1部分,重点介绍并行压缩机的概念,方法学的理论和局限性;第二篇论文,第2部分[1]介绍了近似方法的应用,并与实验数据。

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