Sensitive Flutter Parameters Analysis with Respect to Flutter-Free Design of Compressor Blade

摘要：

　　As the mission requirements of the aero engine improve,the blade aerodynamic loading is higher,especially for lightweight designed blade.The possibility of the blade self-excited vibration increases,so flutter becomes one of the problems for fan and compressor design.However,there is no flutter related parameters in engineering as a reference for compressor flutter-free design until now.That is why the sensitive flutter parameters were studied which could suppress the flutter.

关键词： flutter compressor energy method sensitive flutter parameter flutter-free design

作者: Sun Hai Yang Lin Li Hongxin

作者单位: AVIC Shenyang Engine Design and Research Institute,Shenyang,110015,P.R.China

会议类型: 国际会议

会议名称: 2014 Asia-Pacific International Symposium on Aerospace Technology(2014亚太航空航天技术学术会议)

会议地点: 上海

会议语种:英文

页码: 1-8

在线出版日期: 2014-09-24（万方平台首次上网日期，不代表论文的发表时间）