FLOW GENERATED BY RAMP TABS IN A ROCKET NOZZLE EXHAUST

被引：1
|
作者：
SIMMONS, JM
GOURLAY, CM
LESLIE, BA
机构：
来源：
JOURNAL OF PROPULSION AND POWER | 1987年 / 3卷 / 01期
关键词：
D O I：
10.2514/3.22959
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：93 / 95
页数：3
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