Non-Dimensional Parameters for Comparing Conventional and Counter-Rotating TurbomachinesSource: Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 012::page 0121006-1DOI: 10.1115/1.4051559Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: Counter-rotating turbomachines have the potential to be high efficiency, high power density devices. Comparisons between conventional and counter-rotating turbomachines in the literature make multiple and often contradicting conclusions about their relative performance. By adopting appropriate non-dimensional parameters, based on relative blade speed, the design space of conventional machines can be extended to include those with counter-rotation. This allows engineers familiar with conventional turbomachinery to transfer their experience to counter-rotating machines. By matching appropriate non-dimensional parameters, the loss mechanisms directly affected by counter-rotation can be determined. A series of computational studies are performed to investigate the relative performance of conventional and counter-rotating turbines (CRTs) with the same non-dimensional design parameters. Each study targets a specific loss source, highlighting which phenomena are directly due to counter-rotation and which are solely due to blade design. The studies range from two-dimensional blade sections to three-dimensional finite radius stages. It is shown that, at hub-to-tip ratios (HTRs) approaching unity, with matched non-dimensional design parameters, the stage efficiency and work output are identical for both types of machines. However, a CRT in the study is shown to have an efficiency advantage over a conventional machine of up to 0.35 percentage points for a HTR of 0.65. This is due to differences in absolute velocity producing different spanwise blade designs.
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contributor author | Waldren, J. J. | |
contributor author | Clark, C. J. | |
contributor author | Grimshaw, S. D. | |
contributor author | Pullan, G. | |
date accessioned | 2022-02-06T05:52:28Z | |
date available | 2022-02-06T05:52:28Z | |
date copyright | 7/5/2021 12:00:00 AM | |
date issued | 2021 | |
identifier issn | 0889-504X | |
identifier other | turbo_143_12_121006.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl1/handle/yetl/4278954 | |
description abstract | Counter-rotating turbomachines have the potential to be high efficiency, high power density devices. Comparisons between conventional and counter-rotating turbomachines in the literature make multiple and often contradicting conclusions about their relative performance. By adopting appropriate non-dimensional parameters, based on relative blade speed, the design space of conventional machines can be extended to include those with counter-rotation. This allows engineers familiar with conventional turbomachinery to transfer their experience to counter-rotating machines. By matching appropriate non-dimensional parameters, the loss mechanisms directly affected by counter-rotation can be determined. A series of computational studies are performed to investigate the relative performance of conventional and counter-rotating turbines (CRTs) with the same non-dimensional design parameters. Each study targets a specific loss source, highlighting which phenomena are directly due to counter-rotation and which are solely due to blade design. The studies range from two-dimensional blade sections to three-dimensional finite radius stages. It is shown that, at hub-to-tip ratios (HTRs) approaching unity, with matched non-dimensional design parameters, the stage efficiency and work output are identical for both types of machines. However, a CRT in the study is shown to have an efficiency advantage over a conventional machine of up to 0.35 percentage points for a HTR of 0.65. This is due to differences in absolute velocity producing different spanwise blade designs. | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Non-Dimensional Parameters for Comparing Conventional and Counter-Rotating Turbomachines | |
type | Journal Paper | |
journal volume | 143 | |
journal issue | 12 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.4051559 | |
journal fristpage | 0121006-1 | |
journal lastpage | 0121006-10 | |
page | 10 | |
tree | Journal of Turbomachinery:;2021:;volume( 143 ):;issue: 012 | |
contenttype | Fulltext |