A Method for Evaluating the Effect of Circumferential Inlet Distortion on the Aerodynamic Stability of Multi-Stage Axial-Flow Compressors
Tsuguji Nakano and Andy Breeze-Stringfellow
2010
会议名称Turbomachinery: Unsteady Flows in Turbomachinery
会议日期2010
内容类型会议论文
源URL[http://ir.etp.ac.cn/handle/311046/22227]  
专题工程热物理研究所_国际学术会议论文_A_会议论文
推荐引用方式
GB/T 7714
Tsuguji Nakano and Andy Breeze-Stringfellow. A Method for Evaluating the Effect of Circumferential Inlet Distortion on the Aerodynamic Stability of Multi-Stage Axial-Flow Compressors[C]. 见:Turbomachinery: Unsteady Flows in Turbomachinery. 2010.
个性服务
查看访问统计
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
暂无评论
 

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。


©版权所有 ©2017 CSpace - Powered by CSpace