SUPERSONIC-FLOW ABOUT CIRCULAR CONES AT LARGE ANGLES OF ATTACK - FLOATING DISCONTINUITY APPROACH

被引：0
|
作者：
DAYWITT, J
KUTLER, P
ANDERSON, D
机构：
[1] NASA,AMES RES CTR,COMPUTAT FLUID DYNAM BRANCH,MOFFETT FIELD,CA 94035
[2] IOWA STATE UNIV,AMES,IA 50011
来源：
ASTRONAUTICS & AERONAUTICS | 1977年 / 15卷 / 10期
关键词：
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
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页码：B8 / B8
页数：1
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