Aero-engine intake aerodynamic design and analysis

航空发动机进气气动设计与分析

• 批准号: 2132623
• 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-2132623
• 关键词: Aero; engine; intake; aerodynamic; design

Previous work at Cranfield University has developed methods for the design of intake aero-lines for podded engine configurations. These tools are being extended to three-dimensional configurations with the ultimate aim of developing a viable short intake for future ultra-high bypass ratio configurations. This related research encompasses the development of optimization methods as well as including the interaction between the fan and the intake using low-order fan models.The overall aim of the PhD research is to develop tools and design guidance in the design of short intakes in association with fan systems for future ultrahigh bypass engine configurations.

克兰菲尔德大学之前的工作已经开发出了为吊舱发动机配置设计进气流线的方法。这些工具正在扩展到三维配置，最终目的是为未来的超高旁路比配置开发可行的短进气口。这项相关的研究包括优化方法的开发，以及使用低阶风扇模型的风扇和进气之间的相互作用。PHD研究的总体目标是开发工具和设计指南，与未来超高旁路发动机配置的风扇系统相关联的短进气口设计。

项目成果

Aerodynamics of a short intake in crosswind

侧风中短进气的空气动力学

• DOI: 10.1016/j.ast.2022.107826
• 发表时间: 2022
• 期刊: Aerospace Science and Technology
• 影响因子: 5.6
• 作者: Boscagli L