Spoiler Aerodynamics and Aeroacoustics

扰流板空气动力学和气动声学

• 批准号: 2906039
• 金额: --
• 依托单位: University of Southampton
• 依托单位国家: 英国
• 项目类别: Studentship
• 财政年份: 2021
• 资助国家: 英国
• 起止时间: 2021 至 无数据
• 项目状态: 未结题
• 来源: https://gtr.ukri.org/projects?ref=studentship-2906039
• 关键词: Spoiler; Aerodynamics; Aeroacoustics

A PhD studentship is now available in the area of aircraft aerodynamics and aeroacoustics noise. The studentship provides a unique opportunity to work on a relevant engineering problem at the Airbus Noise Technology Centre (ANTC), part of the Faculty of Engineering and Physical Sciences at the University of Southampton. The studentship is fully funded via an EU H2020 project entitled INVENTOR "INnoVative dEsign of iNstalled airframe componenTs for aircraft nOise Reduction." The project involves 16 partners from 7 different countries.The primary goal of INVENTOR is to better understand the physics of noise generated by spoilers on the wing and landing gears, both deployed of approach to landing. The research will be through a combination of wind tunnel experiments and numerical simulations. The experiments will be performed using the wind tunnel facilities at the University of Southampton. The numerical simulations will involve traditional CFD solvers and also state-of-the-art Lattice Bolztmann codes. The project will suit a student with strong analytical skills as well as some experience in wind tunnel experiments and CFD. The outcome of the project will be a more fundamental understanding of the underlying aerodynamic mechanisms responsible for the noise sources and the student will be expected to propose creative design solutions for their reduction. This PhD studentship will provide a good opportunity to work closely with one of the largest aerospace companies in the world, and explore relevant problems in the aerospace industry.

目前在飞机空气动力学和航空声学噪声领域提供博士生奖学金。该奖学金提供了一个独特的机会，在南安普顿大学工程和物理科学学院的一部分，空中客车噪声技术中心（ANTC）研究相关的工程问题。该奖学金完全由欧盟H2020项目资助，该项目名为“减少飞机噪音的嵌入式机身部件的创新设计”。“该项目涉及来自7个不同国家的16个合作伙伴。EQUIPTOR的主要目标是更好地了解机翼和起落架上的扰流器产生的噪声的物理特性，两者都是在着陆时部署的。研究将通过风洞实验和数值模拟相结合。实验将使用南安普顿大学的风洞设施进行。数值模拟将涉及传统的CFD求解器和最先进的Lattice Bolztmann代码。该项目将适合具有较强的分析能力以及在风洞实验和CFD的一些经验的学生。该项目的成果将是对噪声源的基本空气动力学机制的更基本的理解，学生将被期望提出创造性的设计解决方案，以减少噪声。这个博士生奖学金将提供一个很好的机会，与世界上最大的航空航天公司之一密切合作，并探讨航空航天工业的相关问题。