A parameteric study of the Busemann biplane phenomena

被引：3

作者：

Igra, D. ^{[1
]}

Arad, E. ^{[1
]}

机构：

[1] RAFAEL, Aerodynam Grp, Haifa, Israel

来源：

SHOCK WAVES | 2007年 / 16卷 / 03期

关键词：

Busemann biplane; Computational Fluid Dynamics (CFD); drag reduction; supersonic flow;

D O I：

10.1007/s00193-006-0070-x

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

This paper presents a numerical investigation of the flow field around a Busemann biplane. Several parameters were investigated numerically in order to find their effect on the drag coefficient of the Busemann biplane at various flow conditions. It was found that under most flow conditions the Busemann biplane has a lower drag coefficient than that of a similar single wing.

引用

页码：269 / 273

页数：5