IMPROVED BLADE PROFILE LOSS AND DEVIATION ANGLE MODELS FOR ADVANCED TRANSONIC COMPRESSOR BLADINGS: PART II -A MODEL FOR SUPERSONIC FLOW
W.M. König ; D.K. Hennecke ; L.Fottner
1994
会议名称ASME
会议日期1994-06-13
会议地点The Hague, Netherlands
学科主题Presented at the International Gas Turbine and Aeroengine Congress
内容类型会议论文
源URL[http://ir.etp.ac.cn/handle/311046/40740]  
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
W.M. König,D.K. Hennecke,L.Fottner. IMPROVED BLADE PROFILE LOSS AND DEVIATION ANGLE MODELS FOR ADVANCED TRANSONIC COMPRESSOR BLADINGS: PART II -A MODEL FOR SUPERSONIC FLOW[C]. 见:ASME. The Hague, Netherlands. 1994-06-13.
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