Engineering Fellowships for Growth: Materials by Design for Impact in Aerospace Engineering

工程奖学金促进增长：材料设计对航空航天工程的影响

• 批准号: EP/M002322/2
• 负责人: Hyunsun Kim
• 金额: $ 120.55万
• 依托单位: CARDIFF UNIVERSITY
• 依托单位国家: 英国
• 项目类别: Fellowship
• 财政年份: 2015
• 资助国家: 英国
• 起止时间: 2015 至 无数据
• 项目状态: 已结题
• 来源: https://gtr.ukri.org/projects?ref=EP%2FM002322%2F2
• 关键词: Engineering; Fellowships; Growth; Materials; Design

Policy makers and regulatory bodies are demanding the aerospace industry reduces CO2 emission by 50% and NOx emission by 80% by 2020. In order to meet these drastic demands and ensure affordable air travel in the future, it is essential to make lighter aircraft which will use minimum fuel. The aerospace research community recognises the need to make a dramatic performance improvement and is considering several new aircraft concepts that move away from the conventional two-wing-one-fuselage configuration. This brings new challenges to aircraft design. A wing is a highly complex structure to design as it needs to consider the complex interaction between aerodynamics and structural behaviour. The current design practice is therefore very much based on using the previous successful design data. The challenge of departing from the conventional aircraft is that there are limited successful historical design data that is applicable to new concept aircraft. Once we have a wing design, however, there are sophisticated computational methods that analyse how the wing behaves under external flight conditions.In fact, there has been a significant level of development in computational analysis methods taking advantage of growing computational power. A prime example of this is the recent development in the computational modelling of materials. Using this technology, new advanced materials can be created in half the time that traditional material development takes and the return on investment in computational materials research has been estimated at between 300 - 900%.This fellowship is at the heart of developing sophisticated computational methods to design aircraft configurations that have not been considered before. The majority of the current methods analyse how a given material or structure responds to the external environment such as in flight at speed Mach 0.8, 38000 ft. What is different about the methods in this research is that they are inverse of the analysis methods: They will determine the best combination of advanced material and structural configuration based on the external environment and hence design the optimum wing for the given flight conditions. My research approach is to represent the design problem as a set of mathematical functions and develop computational methods to find the optimum solution. The methods will therefore, find the optimum design for both materials and structural configuration at the same time. The outcome of this fellowship will provide engineers with a sophisticated tool to design complex aircraft structures. The tools will be developed and disseminated in a way that they can be used on a range of other complex engineering problems.The UK has 17% of the global aerospace market share with revenue of £24 billion and is responsible for 3.6% national employment. With the international civil aerospace market forecast to grow to $4 trillion by 2030, the UK market has the opportunity to grow to $352 billion by 2030. It is critical that the UK develops this unique capability to ensure we maintain the market share of these high value products and processes and its economy has the opportunity for growth. Furthermore, the weight savings which will be made from optimum use of materials lead to meeting the emission targets, thus ensuring sustainable environment for the future generations.

政策制定者和监管机构要求航空航天业到2020年将二氧化碳排放量减少50%，氮氧化物排放量减少80%。为了满足这些巨大的需求，并确保未来的航空旅行负担得起，必须制造更轻的飞机，使用最少的燃料。航空航天研究界认识到有必要进行显着的性能改进，并正在考虑几种新的飞机概念，摆脱传统的两翼单机身配置。这给飞机设计带来了新的挑战。机翼是一个高度复杂的结构设计，因为它需要考虑空气动力学和结构行为之间的复杂相互作用。因此，目前的设计实践在很大程度上是基于使用以前成功的设计数据。脱离传统飞机的挑战在于，适用于新概念飞机的成功的历史设计数据有限。然而，一旦我们有了机翼设计，就有了复杂的计算方法来分析机翼在外部飞行条件下的行为。事实上，利用不断增长的计算能力，计算分析方法已经有了很大的发展。这方面的一个主要例子是材料计算建模的最新发展。利用这项技术，可以在传统材料开发的一半时间内创建新的先进材料，并且计算材料研究的投资回报率估计在300 - 900%之间。该奖学金是开发复杂计算方法的核心，用于设计以前没有考虑过的飞机构型。目前的大多数方法分析给定的材料或结构如何响应外部环境，例如在以0.8马赫，38000英尺的速度飞行时。与以往的分析方法不同的是，本研究的方法与分析方法相反：根据外部环境确定先进材料和结构构型的最佳组合，从而设计出给定飞行条件下的最佳机翼。我的研究方法是将设计问题表示为一组数学函数，并开发计算方法来找到最佳解决方案。因此，该方法将同时找到材料和结构配置的最佳设计。该奖学金的成果将为工程师提供设计复杂飞机结构的先进工具。这些工具将以一种可以用于一系列其他复杂工程问题的方式开发和传播。英国拥有全球17%的航空航天市场份额，收入240亿英镑，并承担3. 6%的全国就业。预计到2030年，国际民用航空航天市场将增长至4万亿美元，英国市场有机会到2030年增长至3520亿美元。至关重要的是，英国发展这种独特的能力，以确保我们保持这些高价值产品和工艺的市场份额，并确保其经济有增长的机会。此外，通过最佳使用材料来减轻重量，从而达到排放目标，从而为子孙后代确保可持续的环境。

项目成果

Stress constrained optimization using SLP level set topology optimization method

使用SLP水平集拓扑优化方法进行应力约束优化

• 发表时间: 2015
• 作者: Brampton CJ

New optimization method for steered finer composites using the level set method

使用水平集方法引导更精细复合材料的新优化方法

• 发表时间: 2015
• 期刊: Structural and Multidisciplinary Optimization
• 影响因子: 3.9
• 作者: Brampton CJ

Design of stiffened panels for stress and buckling via topology optimization

• DOI: 10.1007/s00158-021-03062-3
• 发表时间: 2021-10-12
• 期刊: STRUCTURAL AND MULTIDISCIPLINARY OPTIMIZATION
• 影响因子: 3.9
• 作者: Chu, Sheng;Featherston, Carol;Kim, H. Alicia
• 通讯作者: Kim, H. Alicia

Microstructural Stress Shape Optimization Using the Level Set Method

• DOI: 10.1115/1.4047152
• 发表时间: 2020-06
• 期刊: Journal of Mechanical Design
• 影响因子: 3.3
• 作者: R. Picelli;S. Townsend;H. Kim

Modern Piezoelectric Energy-Harvesting Materials

• DOI: 10.1007/978-3-319-29143-7
• 发表时间: 2016-03
• 作者: C. Bowen;V. Topolov;H. Kim