经典转子设计的解析和数值解

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE Progress in Aerospace Sciences Pub Date : 2022-04-01 DOI:10.1016/j.paerosci.2021.100793
J.N. Sørensen , V. Okulov , N. Ramos-García
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引用次数: 2

摘要

大约一个世纪以前,Joukowsky(1912-1918)和Betz(1919)提出了两种不同的转子模型。这两种模型都是基于尾流涡结构及其在旋翼面上的感应的假设。然而,由于将尾流行为制定为转子几何气动设计的实际指导方针的复杂性,这些模型直到现在还没有被用于设计实际的工业风力涡轮机转子。本文提出了一种解析求解两种模型的感应问题的方法,为风电机组转子的设计提供了理论依据。我们简要地介绍了两种转子模型背后的理论,并展示了如何利用这一理论来进行转子平台的实际设计,即弦和扭分布。设计了针对不同叶尖速比进行优化的三叶转子,并将其性能与叶片单元/动量技术和升力线理论的结果进行了比较分析。
本文章由计算机程序翻译,如有差异,请以英文原文为准。

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Analytical and numerical solutions to classical rotor designs

About a century ago, two different rotor models were proposed by Joukowsky (1912–1918) and Betz (1919). Both models were based on assumptions regarding the vortex structures of the wake and its induction on the rotor plane. However, due to complications of formulating the wake behavior into actual guidelines for the aerodynamic design of the rotor geometry, the models have until now not been used to design actual industrial wind turbine rotors. In this article, we propose a technique to solve analytically the induction problem of the two models, which enables the design of wind turbine rotors. We briefly present the theory behind the two rotor models, and show how this theory can be exploited to make actual designs of rotor planforms, i.e. chord- and twist-distributions. The designs are for three-bladed rotors optimized for different tip speed ratios and analyzed by comparing their performance to results using blade-element/momentum technique and lifting line theory.

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来源期刊
Progress in Aerospace Sciences
Progress in Aerospace Sciences 工程技术-工程:宇航
CiteScore
20.20
自引率
3.10%
发文量
41
审稿时长
5 months
期刊介绍: "Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information. The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.
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