Aero-engine intake aerodynamic design, optimisation and test

航空发动机进气气动设计、优化与试验

• 批准号: 2199135
• 金额: --
• 依托单位: CRANFIELD UNIVERSITY
• 依托单位国家: 英国
• 项目类别: Studentship
• 财政年份: 2018
• 资助国家: 英国
• 起止时间: 2018 至 无数据
• 项目状态: 已结题
• 来源: https://gtr.ukri.org/projects?ref=studentship-2199135
• 关键词: Aero; engine; intake; aerodynamic; design

With the continuing need for new air vehicle systems with aero-engines there is a need to the closer integration of the propulsion system and the airframe. With the timely development of new measurement methods, computational tools and optimisation systems it is envisaged that this design challenge can be addressed. The overall aim of the PhD project is to develop, validate and transfer an aerodynamic design and optimisation methodology for complex aero engine intakes. The project is in collaboration with the UK Defence Science and Technology Laboratory and is fully funded for fees and bursary.

随着对具有航空发动机的新型飞行器系统的持续需求，需要推进系统和机身更紧密地结合。随着新的测量方法、计算工具和优化系统的及时开发，可以预见这一设计挑战可以得到解决。博士项目的总体目标是为复杂的航空发动机进气道开发，验证和转移空气动力学设计和优化方法。该项目是与英国国防科学技术实验室合作，并充分资助的费用和奖学金。