水轮机转轮后流速分布的室内模拟方法2。方法验证

IF 0.5 4区 工程技术 Q4 MECHANICS
A. S. Ustimenko, I. V. Litvinov, V. I. Sonin, S. I. Shtork, P. A. Kuibin, A. V. Semenova
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引用次数: 0

摘要

本文介绍了一种对水轮机尾水管入口流速分布进行建模的方法,该方法可以显著降低试验成本。流动是用一个特殊的旋涡组成的组合两排叶片:固定和旋转。利用前人提出的旋流器生成与真实水轮机后速度分布相对应的速度场的设计方法,设计了8排叶片,模拟了不同类型水轮机最优运行模式下的速度分布。本文利用Ansys程序对气流参数进行了数值计算,并将设计速度分布与在气动装置上用激光多普勒风速仪得到的实验速度分布进行了比较。设计、计算和实验结果表明,尾水管入口的流速曲线是令人满意的。由此,成功地验证了一种有前途的水轮机流动实验建模方法。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

APPROACH TO THE LABORATORY MODELING OF THE FLOW VELOCITY DISTRIBUTION BEHIND HYDRO-TURBINE RUNNER 2. VERIFICATION OF THE METHOD

APPROACH TO THE LABORATORY MODELING OF THE FLOW VELOCITY DISTRIBUTION BEHIND HYDRO-TURBINE RUNNER 2. VERIFICATION OF THE METHOD

This paper describes an approach to modeling the flow velocity distribution at the inlet of the hydro turbine draft tube that can significantly reduce test costs. The flow is modeled using a special swirler consisting of a combination of two blade rows: fixed and rotating. The previously proposed method for designing swirlers to generate velocity fields corresponding to the velocity distributions behind real hydro turbines was used to design eight blade rows modeling the velocity distributions in optimal operating modes of hydro turbines of various types. This paper presents a test numerical calculation of the flow parameters using Ansys code and a comparison of design velocity distributions with experimental velocity profiles obtained on an aerodynamic rig using a laser Doppler anemometer. The design, calculated, and experimental flow velocity profiles at the draft tube inlet are shown to be in satisfactory agreement. Thus, the promising approach to the experimental modeling of hydro turbine flow was successfully tested.

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来源期刊
CiteScore
1.20
自引率
16.70%
发文量
43
审稿时长
4-8 weeks
期刊介绍: Journal of Applied Mechanics and Technical Physics is a journal published in collaboration with the Siberian Branch of the Russian Academy of Sciences. The Journal presents papers on fluid mechanics and applied physics. Each issue contains valuable contributions on hypersonic flows; boundary layer theory; turbulence and hydrodynamic stability; free boundary flows; plasma physics; shock waves; explosives and detonation processes; combustion theory; multiphase flows; heat and mass transfer; composite materials and thermal properties of new materials, plasticity, creep, and failure.
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