Linear stability theory applied to boundary layers

被引:234
|
作者
Reed, HL [1 ]
Saric, WS [1 ]
Arnal, D [1 ]
机构
[1] OFF NATL ETUD & RECH AEROSP, CTR ETUD & RECH TOULOUSE, DEPT AEROTHERMODYNAM, F-31055 TOULOUSE, FRANCE
关键词
laminar flow control; drag reduction; transition;
D O I
10.1146/annurev.fl.28.010196.002133
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
The objective of this review is to provide a critical evaluation of linear stability theory for wall-bounded shear flows, with an emphasis on results, not techniques. The results deal with applications to different flowfields related to aircraft systems. Because the flight condition is usually a low-disturbance environment, stability plays an important role in the transition process. Linear stability theory is not a new topic, so emphasis is placed on the most recent accomplishments.
引用
收藏
页码:389 / 428
页数:40
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