contributor author | Xiaohua Wu | |
contributor author | Paul A. Durbin | |
date accessioned | 2017-05-09T00:03:37Z | |
date available | 2017-05-09T00:03:37Z | |
date copyright | July, 2000 | |
date issued | 2000 | |
identifier issn | 0889-504X | |
identifier other | JOTUEI-28679#442_1.pdf | |
identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/124462 | |
description abstract | Turbulent wakes swept across a flat plate boundary layer simulate the phenomenon of wake-induced bypass transition. Benchmark data from a direct numerical simulation of this process are presented and compared to Reynolds-averaged predictions. The data are phase-averaged skin friction and mean velocities. The predictions and data are found to agree in many important respects. One discrepancy is a failure to reproduce the skin friction overshoot following transition. [S0889-504X(00)00503-1] | |
publisher | The American Society of Mechanical Engineers (ASME) | |
title | Boundary Layer Transition Induced by Periodic Wakes | |
type | Journal Paper | |
journal volume | 122 | |
journal issue | 3 | |
journal title | Journal of Turbomachinery | |
identifier doi | 10.1115/1.1303076 | |
journal fristpage | 442 | |
journal lastpage | 449 | |
identifier eissn | 1528-8900 | |
keywords | Flow (Dynamics) | |
keywords | Turbulence | |
keywords | Wakes | |
keywords | Boundary layers | |
keywords | Computation AND Skin friction (Fluid dynamics) | |
tree | Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003 | |
contenttype | Fulltext | |