4.6 Article

Ferrofluid moving thin films for active flow control

期刊

CHINESE JOURNAL OF AERONAUTICS
卷 34, 期 5, 页码 115-119

出版社

ELSEVIER SCIENCE INC
DOI: 10.1016/j.cja.2020.11.008

关键词

Active flow control; Boundary layer separation; Ferrofluid

资金

  1. Spanish Ministry of Economy and Competitiveness under Fellowship Grant Ramon y Cajal [RYC-2013-13459]

向作者/读者索取更多资源

The study discusses the potential significance of using ferrofluid moving thin films for lift and attack angle enhancement. By attaching a thin film of ferrofluid to the wing wall and pumping it tangentially along the wing, lift enhancement and changes in the attack angle can be achieved. Further research and design are needed to explore the possibilities of using ferrofluid moving thin films.
Ferrofluid moving thin films and their possible significance with regard to active flow control for lift and attack angle enhancement are discussed. In this strategy, a very thin film of ferrofluid is strongly attached at the wall of the wing by a normal magnetic field from below and pumped tangentially along the wing. Utilizing a simplified physical model and from the available experimental data on moving walls, the expected lift enhancement and effect on the attack angle were assessed. Additional research and design is required in order to explore the possibilities in the use of ferrofluid moving thin films. (c)& nbsp;2021 Chinese Society of Aeronautics and Astronautics. Production and hosting by Elsevier Ltd. This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/).

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