Linear evolution of controlled disturbances in the supersonic boundary layer on a swept wing |
| |
| Authors: | Yu G Ermolaev G L Kolosov A D Kosinov N V Semenov |
| |
| Institution: | 1. Khristianovich Institute of Theoretical and Applied Mechanics, ul. Institutskaya 4/1, Novosibirsk, 630090, Russia
|
| |
| Abstract: | The linear development of controlled disturbances in the three-dimensional supersonic boundary layer on a swept model wing with a sharp leading edge is experimentally investigated at the Mach number 2. The spatial-temporal and spectral-wave characteristics of the wave train of unstable disturbances are obtained. The asymmetry of these characteristics, due to the secondary flow in the three-dimensional boundary layer, is confirmed. |
| |
| Keywords: | |
| 本文献已被 SpringerLink 等数据库收录！ |
|
