FLOW COMPUTATIONS IN INLETS AT INCIDENCE USING A SHOCK FITTING BICHARACTERISTIC METHOD

被引：3
|
作者：
VADYAK, J [1 ]
HOFFMAN, JD [1 ]
BISHOP, AR [1 ]
机构：
[1] NASA,LEWIS RES CTR,DIV WIND TUNNEL & FLIGHT,AERODYNAM ANAL SECT,CLEVELAND,OH 44135
来源：
AIAA JOURNAL | 1980年 / 18卷 / 12期
关键词：
D O I：
10.2514/3.50910
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：1495 / 1502
页数：8
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