EFFECT OF STREAM SURFACE CONVERGENCE ON TURBOMACHINE BLADE BOUNDARY-LAYERS

被引：0

作者：

DUNHAM, J ^{[1
]}

机构：

[1] NATL GAS TURBINE ESTAB,FARNBOROUGH,ENGLAND

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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

页码：90 / 92

页数：3

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