旋翼动态失速研究进展:实验与流动控制

IF 11.5 1区 工程技术 Q1 ENGINEERING, AEROSPACE
Anthony D. Gardner , Anya R. Jones , Karen Mulleners , Jonathan W. Naughton , Marilyn J. Smith
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引用次数: 5

摘要

50多年来,动态失速一直是一个技术挑战,也是一个令人感兴趣的流体动力学主题;但在过去的十年里,在对转子动态失速的理解、预测、建模和控制方面取得了重大进展。本文概述了动态失速实验的现状,以及理解转子动态失速的未来方向。讨论了实验数据集,以及动态失速控制的未来研究方向。翼型和旋转叶片之间的协调测试,以及计算和实验研究之间的紧密结合被发现是富有成效的方法。先进的分析方法,包括统计方法、模态表示和人工智能方法,在理解动态失速方面取得了重大进展。对动态失速控制装置的研究已经允许对向分离流的过渡进行许多有用的有针对性的研究,但尚未产生商业化实施的装置。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Review of rotating wing dynamic stall: Experiments and flow control

Dynamic stall has been a technical challenge and a fluid dynamical subject of interest for more than fifty years; but in the last decade significant advances have been made in the understanding, prediction, modeling, and control of dynamic stall on rotors. This paper provides a summary of the state of the art of dynamic stall experiments and future directions in the understanding of dynamic stall on rotors. Experimental data sets are discussed, as well the direction of future research for control of dynamic stall. Coordinated testing between airfoils and rotating blades, as well as close integration between computational and experimental studies were found to be productive approaches. Advanced analysis methods, including statistical methods, modal representations, and artificial intelligence methods have led to significant advances in the understanding of dynamic stall. Investigations of dynamic stall control devices have allowed many useful targeted investigations of the transition to separated flow, but have not yet resulted in a commercially implemented device.

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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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