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Experimental study on thermal efficiency of a multi-jet anti-icing system with piccolo tube

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

An experimental study was conducted to investigate the jet impingement thermal efficiency of a typical model for a multijet anti-icing system under different experimental conditions such as air mass flow rate at the jet exit, piccolo tube position and circumferential angle of jet holes. The experimental results showed that jet mass flow rate, velocity at the jet exits (whether choking conditions were established at the jet exits or not) and piccolo tube-to-leading edge distance within the cavity had significant influence on thermal efficiency of the anti-icing system. The heat flux on the external surface of leading edge, diameter of jet holes and circumferential angle of jet holes had a measurable but small effect on thermal efficiency of the anti-icing system.

源语言英语
主期刊名Turbomachinery
出版商American Society of Mechanical Engineers (ASME)
ISBN(电子版)9780791884072
DOI
出版状态已出版 - 2020
活动ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020 - Virtual, Online
期限: 21 9月 202025 9月 2020

出版系列

姓名Proceedings of the ASME Turbo Expo
2B-2020

会议

会议ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, GT 2020
Virtual, Online
时期21/09/2025/09/20

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