Study of the Effect of the Depth of the Cavity of a Braking Device on the Aerodynamic Drag of a Model in Transonic and Supersonic Flow

被引:0
|
作者
N. N. Pilyugin
V. S. Khlebnikov
机构
来源
Fluid Dynamics | 2005年 / 40卷
关键词
Mach number; transonic flow; supersonic flow; aerodynamic drag coefficient; cavity depth; flow pattern;
D O I
暂无
中图分类号
学科分类号
摘要
The flowfield and the aerodynamic drag of a model consisting of a pair of bodies (leading body a cylinder and trailing body a hollow cylinder) connected by a cylindrical bar along the axis of symmetry is experimentally investigated at Mach numbers ranging from 0.6 to 1.7. In the course of the experiments, the trailing body cavity depth and the connecting bar length were varied.
引用
收藏
页码:332 / 337
页数:5
相关论文
共 32 条