Control of a swept-wing boundary layer perturbed by free-stre am turbulence
受自由流湍流扰动的后掠翼边界层的控制
基本信息
- 批准号:EP/I033173/1
- 负责人:
- 金额:$ 12.72万
- 依托单位:
- 依托单位国家:英国
- 项目类别:Research Grant
- 财政年份:2011
- 资助国家:英国
- 起止时间:2011 至 无数据
- 项目状态:已结题
- 来源:
- 关键词:
项目摘要
Wall suction has been used extensively to reduce the growth of laminar boundary layer disturbances, such as Tollmien-Schlichting waves, cross-flow vortices and, more recently, Klebanoff modes, namely unsteady streamwise-elongated low-frequency disturbances generated by free-stream vortical perturbations. Wall suction has resulted in a delay of transition to turbulence with major benefits, such as reduction of viscous drag, noise, and fuel consumption.The central aim of the proposed work is to apply wall suction to attenuate the intensity of Klebanoff modes arising in swept-wing laminar boundary layers due to free-stream turbulence. These flow structures have never been studied over large scale aerodynamic bodies, despite their vast importance in numerous industrial and technological applications, such as the design of aircraft wings and turbine blades. The effects of wall suction have not been investigated for these technologically relevant flows. A reason for the dearth of works is the extreme difficulty in predicting and controlling such flows.The problem will be tackled by a combination of mathematical and numerical techniques. The proposed approach will offer a fast and numerically robust toolkit in line with the long-standing effort of the fluid mechanics community to control pre-transitional flows in an efficient manner.
壁吸力已被广泛用于减少层流边界层扰动的增长,例如 Tollmien-Schlichting 波、交叉流涡流以及最近的 Klebanoff 模式,即由自由流涡旋产生的不稳定流向伸长低频扰动扰动。壁吸力导致了向湍流过渡的延迟,带来了重大好处,例如减少粘性阻力、噪音和燃料消耗。拟议工作的中心目标是应用壁吸力来减弱扫掠中产生的 Klebanoff 模式的强度- 由于自由流湍流而产生的机翼层流边界层。尽管这些流动结构在许多工业和技术应用中非常重要,例如飞机机翼和涡轮叶片的设计,但从未在大型空气动力体上进行过研究。对于这些技术相关的流动,尚未研究壁吸力的影响。缺乏相关工作的一个原因是预测和控制此类流动极其困难。该问题将通过数学和数值技术的结合来解决。所提出的方法将提供一个快速且数值稳健的工具包,符合流体力学界长期以来为有效控制过渡前流动所做的努力。
项目成果
期刊论文数量(4)
专著数量(0)
科研奖励数量(0)
会议论文数量(0)
专利数量(0)
Streamwise-travelling viscous waves in channel flows.
河道流动中沿河道行进的粘性波。
- DOI:http://dx.10.1007/s10665-018-9953-y
- 发表时间:2018
- 期刊:
- 影响因子:1.3
- 作者:Ricco P
- 通讯作者:Ricco P
Laminar Streaks in Oscillating Boundary Layers
振荡边界层中的层流条纹
- DOI:http://dx.10.1016/j.piutam.2015.03.049
- 发表时间:2015
- 期刊:
- 影响因子:0
- 作者:Hicks P
- 通讯作者:Hicks P
Laminar streak growth above a spanwise oscillating wall
展向振荡壁上方的层流条纹生长
- DOI:http://dx.10.1017/jfm.2015.98
- 发表时间:2015
- 期刊:
- 影响因子:3.7
- 作者:Hicks P
- 通讯作者:Hicks P
Growth of boundary-layer streaks due to free-stream turbulence
由于自由流湍流而导致边界层条纹的增长
- DOI:http://dx.10.1016/j.ijheatfluidflow.2016.05.003
- 发表时间:2016
- 期刊:
- 影响因子:2.6
- 作者:Ricco P
- 通讯作者:Ricco P
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Pierre Ricco其他文献
Impact of vacuum degree on the aerodynamics of a high-speed train capsule running in a tube
真空度对高速列车舱管内运行空气动力学的影响
- DOI:
10.1016/j.ijheatfluidflow.2020.108752 - 发表时间:
2021 - 期刊:
- 影响因子:2.6
- 作者:
Yang Sui;Jiqiang Niu;Pierre Ricco;Qiujun Yu;Yanping Yuan;Xiaoling Cao;Xiaofeng Yang - 通讯作者:
Xiaofeng Yang
Görtler Instability and Transition in Compressible Flows
可压缩流动中的 Görtler 不稳定性和转变
- DOI:
10.2514/1.j062866 - 发表时间:
2023-12-29 - 期刊:
- 影响因子:2.5
- 作者:
Dongdong Xu;Pierre Ricco;Lian Duan - 通讯作者:
Lian Duan
Pierre Ricco的其他文献
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{{ truncateString('Pierre Ricco', 18)}}的其他基金
CBET-EPSRC: Transition and Turbulence in Compressible Boundary Layers Subjected to Concave Surface Curvature
CBET-EPSRC:受凹面曲率影响的可压缩边界层中的转变和湍流
- 批准号:
EP/T01167X/1 - 财政年份:2021
- 资助金额:
$ 12.72万 - 项目类别:
Research Grant
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Lift Management for Unsteady Translating Wings Using a Rotating, Swept Wing Tip
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