Quiet aerofoils of the next generation

下一代静音翼型

• 批准号: EP/N018737/1
• 负责人: Tze Chong
• 金额: $ 32.47万
• 依托单位: Brunel University London
• 依托单位国家: 英国
• 项目类别: Research Grant
• 财政年份: 2016
• 资助国家: 英国
• 起止时间: 2016 至 无数据
• 项目状态: 已结题
• 来源: https://gtr.ukri.org/projects?ref=EP%2FN018737%2F1
• 关键词: Quiet; aerofoils; next; generation

Abstracts are not currently available in GtR for all funded research. This is normally because the abstract was not required at the time of proposal submission, but may be because it included sensitive information such as personal details.

目前GtR中并没有提供所有资助研究的摘要。这通常是因为在提交提案时不需要摘要，但也可能是因为它包含敏感信息，如个人详细信息。

项目成果

Optimization of the poro-serrated trailing edges for airfoil broadband noise reduction.

• DOI: 10.1121/1.4961362
• 发表时间: 2016-08
• 期刊: The Journal of the Acoustical Society of America
• 作者: T. Chong;E. Dubois

Reconstruction of the Deterministic Turbulent Boundary Layer for the Study of Aerofoil Self-Noise Mechanisms in the Spatial, Temporal and Frequency Domains

重建确定性湍流边界层以研究机翼时空频域自噪声机制

• DOI: 10.2514/6.2022-2845
• 发表时间: 2022
• 作者: Chong T

Leading Edge Blowing to Mimic and Enhance the Serration Effects for Aerofoil

前缘吹气可模拟并增强机翼的锯齿效应

• DOI: 10.3390/app11062593
• 发表时间: 2021
• 期刊: Applied Sciences
• 作者: Al-Okbi Y

Mimicking the serration effects on aerofoil by leading edge blowing

通过前缘吹气模拟机翼上的锯齿效应

• DOI: 10.2514/6.2018-3287
• 发表时间: 2018
• 作者: Al-Okbi Y

On the noise reduction mechanisms of porous aerofoil leading edges

多孔翼型前缘降噪机理研究

• DOI: 10.1016/j.jsv.2020.115574
• 发表时间: 2020
• 期刊: Journal of Sound and Vibration
• 影响因子: 4.7
• 作者: Chaitanya P