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：

Aerospace engineering;

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

页码：123 / 125

页数：3

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