Computational Study on the Flow Structure of the Prandtl-D Flying Wing

被引：0
|
作者：
Hammer, Patrick R. [1 ]
Garmann, Daniel J. [1 ]
机构：
[1] Air Force Res Lab, Wright Patterson Air Forc, OH 45433 USA
来源：
AIAA JOURNAL | 2024年 / 62卷 / 05期
关键词：
Aircraft Wing Design; Freestream Conditions; Vortex Dynamics; Aerodynamic Performance; Inviscid Flow; NASA; Boundary Layers; Flight Testing; Longitudinal Static Stability; Transport Aircraft;
D O I：
10.2514/1.J063668
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
Journal article (JA)
引用
收藏
页码：1970 / 1973
页数：4
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