Experimental studies and control of wall-bounded and separated shear layers using active flow control

使用主动流动控制对壁限和分离剪切层进行实验研究和控制

• 批准号: RGPIN-2019-07108
• 负责人: Lavoie, Philippe
• 金额: $ 3.35万
• 依托单位: University of Toronto
• 依托单位国家: 加拿大
• 项目类别: Discovery Grants Program - Individual
• 财政年份: 2019
• 资助国家: 加拿大
• 起止时间: 2019-01-01 至 2020-12-31
• 项目状态: 已结题
• 来源: https://www.nserc-crsng.gc.ca/ase-oro/Details-Detailles_eng.asp?id=689274
• 关键词: Experimental; studies; control; wall; bounded

The aerospace sector plays an important role in the Canadian economy. In 2017, it accounted for approximately $25 billion in GDP and nearly 190,000 high-paying jobs. In the specific case of aviation, climate change and noise pollution represents some of its most significant challenges and are risks to the industry. In order for the Canadian aerospace industry to remain globally competitive, step changes in technology are required. Active flow control is one of the technologies considered to help meet the stringent environmental targets set on the aerospace industry by the International Air Transport Association (IATA).******The proposed research will development and implementation novel active flow control strategies with an emphasis on flow fields that are relevant to the Canadian aerospace industry. Specific active flow control objectives to be investigated are: (i) reduction of skin-friction drag due to turbulent boundary layers, and (ii) wake control to decrease the pressure drag and noise emissions from blunt trailing edge airfoils. ******(1) Previous studies demonstrated ~30% reduction in skin friction in turbulent boundary layers through active control of the near-wall turbulence. However, recent works suggests that these benefits would not scale to flight Reynolds number. A new approach of controlling the turbulent boundary layer through the manipulation of the large coherent structures present in the log-region will be considered with this proposal. These structures are known to become more dominant at large Reynolds number and can offer a more practical pathway to implementation given their larger sizes compared to the near-wall structures. ******(2) Airfoils with blunt trailing edges are common in the aerospace industry since they can provide superior lift to drag ratios and improved structural integrity. However, the wake associated with these causes higher levels of pressure drag, fluctuating aerodynamic forces and noise. Preliminary studies by the applicant with a blunt trailing edge streamlined body demonstrated an effective active flow control methodology that produced a reduction in pressure drag of approximately 30% and over 90% less unsteadiness in the wake. It is proposed to take this methodology closer to industrial application by extending its use to blunt trailing edge airfoils. This will lead to significant better performance for these airfoils.******The practical ramifications of this research are significant and wide ranging. They include the reduction of drag, fuel consumption and noise emissions in a variety of commercially relevant fluid systems. These benefits will lead to a reduction in the aerospace industry's dependence on fossil fuels and a decrease in greenhouse gas emissions. The research is also transformative since it addresses open questions that, in the long term, should lead to a paradigm shift with respect to the design practices for energy efficiency of, and pollution reduction from, fluidic systems.**

航空航天部门在加拿大经济中发挥着重要作用。2017年，它占国内生产总值约250亿美元，提供近19万个高薪工作岗位。在航空业的具体案例中，气候变化和噪音污染是该行业面临的一些最重大挑战和风险。为了使加拿大航空航天工业保持全球竞争力，需要逐步改变技术。主动气流控制被认为是帮助满足国际航空运输协会（IATA）对航空航天工业设定的严格环境目标的技术之一。******拟议的研究将开发和实施新的主动流量控制策略，重点是与加拿大航空航天工业相关的流场。要研究的具体主动流动控制目标是：(1)减少湍流边界层造成的表面摩擦阻力，(2)尾迹控制以减少钝尾缘翼型的压力阻力和噪声排放。******(1)以往的研究表明，通过主动控制近壁湍流，湍流边界层的表面摩擦减少了~30%。然而，最近的研究表明，这些好处不会扩展到飞行雷诺数。本文提出了一种新的方法，通过对对数区域中存在的大型相干结构的操纵来控制湍流边界层。已知这些结构在大雷诺数下变得更占优势，并且与近壁结构相比，它们的尺寸更大，可以提供更实用的实现途径。******(2)翼型钝尾缘是常见的航空航天工业，因为他们可以提供优越的升力阻力比和改进的结构完整性。然而，与这些相关的尾流导致更高水平的压力阻力，波动的空气动力和噪音。申请人对钝尾缘流线型体的初步研究表明，有效的主动流动控制方法可以减少约30%的压力阻力，减少90%以上的尾迹不稳定。这是建议采取这种方法更接近工业应用，扩大其使用钝后缘翼型。这将导致显著更好的性能为这些翼型。******这项研究的实际影响是重大而广泛的。它们包括在各种商业相关流体系统中减少阻力、燃油消耗和噪音排放。这些好处将减少航空航天工业对化石燃料的依赖，减少温室气体排放。这项研究也具有变革性，因为它解决了一些悬而未决的问题，从长远来看，这些问题应该会导致流体系统在能效和减少污染的设计实践方面的范式转变