摘要
结合国内外的相关研究工作,对大涵道比涡扇发动机叶轮机部分设计技术研究进展进行了总结和分析,从风扇/压气机设计技术、涡轮设计技术、流动及噪声控制和多学科耦合四个方面阐述了我国发展大涵道比发动机需要解决的部分叶轮机关键技术.
The research progress on partial turbomachinery technology of high-bypassratio turbofan engine were reviewed and analyzed in the present study and the partial key technology of turbomachinery required for our country＇s high-bypass-ratio turbofan engine were also expatiated. The main contents included four aspects： fan/compressor design technique, turbine design technique, flow and noise control and multi-disciplinary coupling technique.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2008年第8期1504-1518,共15页
Journal of Aerospace Power
基金
国家自然科学基金(50776003)
北京航空航天大学蓝天新星计划项目
