Secondary Instability and Subcritical Transition in the Leading-Edge Boundary Layer

被引：0
|
作者：
John, M. O. [1 ]
Obrist, D. [2 ]
Kleiser, L. [1 ]
机构：
[1] Swiss Fed Inst Technol, Inst Fluid Dynam, CH-8092 Zurich, Switzerland
[2] Univ Bern, ARTORG Ctr, CH-3010 Bern, Switzerland
来源：
DIRECT AND LARGE-EDDY SIMULATION X | 2018年 / 24卷
关键词：
STABILITY; SUCTION;
D O I：
10.1007/978-3-319-63212-4_42
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
The leading-edge boundary-layer (LEBL) flow is found in the front part of swept airplane wings where the flow is subject to strong acceleration. © 2018, Springer International Publishing AG.
引用
收藏
页码：333 / 339
页数：7
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