Supersonic Flow around a Body of Small Elongation

被引：0
|
作者：
Guvernyuk, S. V. [1 ]
Zubkov, A. F. [1 ]
Pichkhadze, K. M. [1 ]
Finchenko, V. S. [1 ]
Shvets, A. I. [1 ]
机构：
[1] Moscow MV Lomonosov State Univ, Fac Mech & Math, Leninskie Gory, Moscow 119899, Russia
来源：
MOSCOW UNIVERSITY MECHANICS BULLETIN | 2009年 / 64卷 / 05期
关键词：
D O I：
10.3103/S0027133009050057
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
Some results of experimental studies conducted in a wind tunnel at the Mach number M = 1.78 for a blunt body of small elongation are discussed. The effect of the attack angle on the drag and lift coefficients as well as on the static stability and the pressure center position is considered.
引用
收藏
页码：123 / 125
页数：3
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