Leading-edge shape and aeroengine fan blade performance

被引：0
|
作者：
Sayma, AI
Kim, M
Smith, NHS
机构：
[1] Univ London Imperial Coll Sci Technol & Med, Ctr Vibrat Engn, Dept Mech Engn, London SW7 2BX, England
[2] Rolls Royce PLC, Fan Syst, Derby DE24 8BJ, England
来源：
JOURNAL OF PROPULSION AND POWER | 2003年 / 19卷 / 03期
关键词：
D O I：
暂无
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：516 / 519
页数：4
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