Laminar-Turbulent Transition and Boundary Layer Separation on wavy surface wing

被引：2

作者：

Kozlov, Viktor ^{[1
]}

Zverkov, Ilya ^{[1
]}

Zanin, Boris ^{[1
]}

机构：

[1] Khristianovich ITAM SB RAS, Novosibirsk 630090, Russia

来源：

SEVENTH IUTAM SYMPOSIUM ON LAMINAR-TURBULENT TRANSITION | 2010年 / 18卷

关键词：

D O I：

10.1007/978-90-481-3723-7_89

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

Boundary layer parameters on wavy-surface wings (below wavy wing) at the angle of attack alpha = 0 degrees and the chord Reynolds number Re = 1.7 . 10(5) are studied experimentally. Substantial differences are found in the transition position and in the transition scenarios realized on the wavy-surface wing along its streamwise grooves and humps

引用

页码：517 / 519

页数：3