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Analysis of the transition process around laminar separation bubbles (LSB‘s) in a towing tank using time-resolved 3D particle tracking techniques

Analysis of the transition process around laminar separation bubbles (LSB‘s) in a towing tank using time-resolved 3D particle tracking techniques
使用时间分辨 3D 粒子跟踪技术分析拖曳池中层流分离气泡 (LSBâs) 周围的转变过程
批准号:
422177304
负责人:
Professor Dr. Christian Joachim Kähler
金额:
$0.0万
依托单位国家:
德国
项目类别:
Research Grants
财政年份:
2019
资助国家:
德国
项目状态:
已结题
起止时间:
2018-12-31 至 2023-12-31

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中文摘要
翻译
在较低雷诺数条件下,各种升力表面的性能受到层流边界层分离的显著影响。相关应用的例子包括人造系统,如商用飞机的涡轮风扇发动机叶片和尾部表面,风力涡轮机叶片,以及自然界的飞行员和游泳者。层流边界层分离通常发生在翼型吸力侧,并导致分离剪切层的形成。然后,流动可以经历快速过渡,并在平均意义上重新连接到翼型表面形成层流分离泡(LSB)。由于LSB的改变循环的翼型,因此升力和阻力,整体流动的发展,因此取决于形成和动态的LSB,这是本提案的主要焦点。尽管迄今为止在理解LSB动力学方面取得了重大的研究进展,但在这两个基本重要性的知识方面仍有一些关键的差距有待解决,这是本提案的动机。由于自由流湍流水平对LSB的形成和过渡过程有显著的影响,实验将在一个自由流湍流可以在0到2%之间变化的拖曳通道中进行。此外,复杂的三维时间分辨流量测量技术将用于解决空间和时间上的所有流动过程,具有高特殊分辨率和低测量不确定度。预计这些研究将显著改善目前的知识状况,并且可以可靠地回答开放的研究问题。
英文摘要
The performance of various lifting surfaces at relatively low Reynolds numbers is known to be affected significantly by laminar boundary layer separation. The examples of the relevant application range from man-made systems, such as turbofan engine blades and tail surfaces on commercial aircraft, wind turbine blades, as well as to nature’s flyers and swimmers. The laminar boundary layer separation typically takes place on the suction side of the airfoil and leads to the formation of a separated shear layer. The flow can then undergo rapid transition and be reattached to the airfoil surface in the mean sense forming a Laminar Separation Bubble (LSB). As LSB’s alter the circulation of the airfoil and consequently the lift and drag, the overall flow development therefore depends on the formation and dynamics of the LSB, which are the main focal points of the present proposal. Despite a significant research progress made to date towards understanding LSB dynamics, a number of critical gaps in knowledge of both fundamental importance remain to be addressed, which serves as a motivation for the present proposal. As the free stream turbulence level has a significant effect on the formation of LSB and the transition process, the experiments will be performed in a towing channel whose free stream turbulence can be varied between zero and two percent. Furthermore, sophisticated three-dimensional time-resolved flow measurement techniques will be used to resolve all flow processes in space and time with high special resolution and low measurement uncertainty. It is expected that the studies will significantly improve the current state of knowledge and that open research questions can be reliably answered.
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