SENSITIVITY DERIVATIVES FOR 3-DIMENSIONAL SUPERSONIC EULER CODE USING INCREMENTAL ITERATIVE STRATEGY

被引：3
|
作者：
KORIVI, VM [1 ]
TAYLOR, AC [1 ]
HOU, GW [1 ]
NEWMAN, PA [1 ]
JONES, HE [1 ]
机构：
[1] NASA,LANGLEY RES CTR,DIV FLUID MECH COMPUTAT SCI BRANCH,HAMPTON,VA 23681
来源：
AIAA JOURNAL | 1994年 / 32卷 / 06期
关键词：
Aerodynamic derivatives - Blended wing-body - Euler equations;
D O I：
10.2514/3.12136
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
[No abstract available]
引用
收藏
页码：1319 / 1321
页数：3
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