SUPERSONIC CASCADE TUNNEL USED TO EVALUATE COMPRESSOR BLADE PERFORMANCE

被引：0
|
作者：
STUBNER, AW
CASE, LF
BLAKE, TR
机构：
来源：
JOURNAL OF ENGINEERING FOR POWER | 1966年 / 88卷 / 02期
关键词：
D O I：
10.1115/1.3678498
中图分类号：
TH [机械、仪表工业];
学科分类号：
0802 ;
摘要：
引用
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页码：153 / &
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