Local structure of boundary layer transition in experiments with a single streamwise vortex


Autoria(s): Manu, KV; Dey, J; Mathew, Joseph
Data(s)

2015

Resumo

Transition induced by an isolated streamwise vortex embedded in a flat plate boundary layer was studied experimentally. The vortex was created by a gentle hill with a Gaussian profile that spanned on half of the width of a flat plate mounted in a low turbulence wind tunnel. PIV and hot-wire anemometry data were taken. Transition occurs as a non-inclined shear layer breaks up into a sequence of vortices, close to the boundary layer edge. The passing frequency of these vortices scales with square of the freestream velocity, similar to that in single-roughness induced transition. Quadrant analysis of streamwise and wall-normal velocity fluctuations show large ejection events in the outer layer. (C) 2015 Elsevier Inc. All rights reserved.

Formato

application/pdf

Identificador

http://eprints.iisc.ernet.in/52951/1/Exp_The_Flu_Sci_68_381_2015.pdf

Manu, KV and Dey, J and Mathew, Joseph (2015) Local structure of boundary layer transition in experiments with a single streamwise vortex. In: EXPERIMENTAL THERMAL AND FLUID SCIENCE, 68 . pp. 381-391.

Publicador

ELSEVIER SCIENCE INC

Relação

http://dx.doi.org/10.1016/j.expthermflusci.2015.06.013

http://eprints.iisc.ernet.in/52951/

Palavras-Chave #Aerospace Engineering (Formerly, Aeronautical Engineering)
Tipo

Journal Article

PeerReviewed