TRANSONIC FLOW OVER THE ROOT REGIONS OF BACK- OR FORWARD-SWEPT WINGS.

被引：0

作者：

Nekrasova, M.N. ^{[1
]}

机构：

[1] Zhukovskiy Inst of Aerohydrodynamics, USSR, Zhukovskiy Inst of Aerohydrodynamics, USSR

来源：

Fluid mechanics. Soviet research | 1986年 / 15卷 / 03期

关键词：

FLOW OF FLUIDS - Transonic - MATHEMATICAL TECHNIQUES - Numerical Analysis;

D O I：

暂无

中图分类号：

学科分类号：

摘要：

Results on determination of the pressure distribution on a section of a wing with sweep angle of X equals plus or minus 45 degree at transonic flow velocities are presented. Flow features in a local supersonic zone are analyzed and the pressure drag coefficients of the root sections of back- or forward-swept wings are determined.

引用

页码：33 / 40