| タイトル | Boundary Layer Transition on an Axial Compressor Stator Blade-Wake Passing and Freestream Turbulence Effects |
| 本文（外部サイト） | http://hdl.handle.net/2060/20070038959 |
| 著者（英） | Walker, G. J.; Solomon, W. J. |
| 著者所属（英） | Tasmania Univ. |
| 発行日 | 2007-03-01 |
| 言語 | eng |
| 内容記述 | Quantitative observations of transitional boundary layers in regions of strong flow deceleration on an axial compressor stator blade are reported. Measurements are obtained at a fixed chordwise position, and the blade incidence was varied by changing the compressor throughflow so as to move the transition region relative to the stationary probe. It was thus possible to observe typical boundary layer behavior at various stages of transition in the turbomachine environment. The range of observations covers separating laminar flow at transition onset, and reattachment of intermittently turbulent periodically separated shear layers. |
| NASA分類 | Aerodynamics |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/564815 |
