APPLICATION OF FILM COOLING THEORY TO COOLING OF AIRCRAFT GAS TURBINE CHAMBERS

被引：2
|
作者：
STURGESS, GJ
机构：
来源：
JOURNAL OF THE ROYAL AERONAUTICAL SOCIETY | 1967年 / 71卷 / 678期
关键词：
D O I：
10.1017/S0001924000055524
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：430 / &
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