NAVIER-STOKES INVESTIGATION OF BLUNT TRAILING-EDGE AIRFOILS USING O GRIDS

被引：9
作者：
KHALID, M
JONES, DJ
机构：
[1] High Speed Aerodynamics Laboratory, Institute for Aerospace Research, National Research Council of Canada, Ottawa, ON
来源：
JOURNAL OF AIRCRAFT | 1993年 / 30卷 / 05期
关键词：
D O I：
10.2514/3.46416
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：797 / 800
页数：4
相关论文
共 5 条
[1]  
Stanaway S.K., McCrosky W.J., Kroo I.M., Navier- Stokes Analysis of Blunt Trailing Edge Airfoil, (1992)
[2]  
Chan J.S., Multizone Navier-Stokes Computations of Viscous Transonic Flows around Airfoils, (1988)
[3]  
Drela M., Integral Boundary Layer Formulation for Blunt Trailing Edges, (1989)
[4]  
Pulliam T., Euler and Thin Layer Navier-Stokes Codes: ARC2D and ARC3D, (1984)
[5]  
Khalid M., Jones D.J., A Study of Blunt Trailing Edge Airfoils Using the Navier Stokes Code-ARC2D, Canadian Aeronautics and Space Inst. Conf., (1993)
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