Investigations on controlled transition development in a laminar separation bubble by means of LDA and PIV

When a laminar boundary layer separates because of an adverse streamwise pressure gradient, the flow is subject to increased instability with respect to small-amplitude disturbances. Laminaraturbulent transition occurs under a rapid three-dimensional (3D) development within the separated shear layer...

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Published inExperiments in fluids Vol. 36; no. 1; pp. 43 - 52
Main Authors Rist, U., Lang, M., Wagner, S.
Format Journal Article
LanguageEnglish
Published Heidelberg Springer 01.01.2004
Berlin
Subjects
Online AccessGet full text
ISSN0723-4864
1432-1114
DOI10.1007/s00348-003-0625-x

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Abstract When a laminar boundary layer separates because of an adverse streamwise pressure gradient, the flow is subject to increased instability with respect to small-amplitude disturbances. Laminaraturbulent transition occurs under a rapid three-dimensional (3D) development within the separated shear layer. When the following turbulent boundary layer reattaches, a laminar separation bubble is formed. To allow controlled measurements, a small-amplitude TollmienaSchlichting wave (TS wave) was introduced into the boundary layer without (case I) and with (case II) spanwise forcing of steady 3D disturbances. Combined application of laser-Doppler anemometry (LDA) and particle image velocimetry (PIV) demonstrates the suitability of both measurement techniques to capture the development of unsteady, periodic phenomena. The transition mechanism occurring in the flow field under consideration is discussed, and results obtained by controlled measurements are compared to direct numerical simulations (DNS) and predictions from linear stability theory (LST). Flow visualizations and stereoscopic PIV measurements give better insight into the 3D breakdown of the separated shear layer.
AbstractList When a laminar boundary layer separates because of an adverse streamwise pressure gradient, the flow is subject to increased instability with respect to small-amplitude disturbances. Laminar-turbulent transition occurs under a rapid three-dimensional (3D) development within the separated shear layer. When the following turbulent boundary layer reattaches, a laminar separation bubble is formed. To allow controlled measurements, a small-amplitude Tollmien-Schlichting wave (TS wave) was introduced into the boundary layer without (case I) and with (case II) spanwise forcing of steady 3D disturbances. Combined application of laser-Doppler anemometry (LDA) and particle image velocimetry (PIV) demonstrates the suitability of both measurement techniques to capture the development of unsteady, periodic phenomena. The transition mechanism occurring in the flow field under consideration is discussed, and results obtained by controlled measurements are compared to direct numerical simulations (DNS) and predictions from linear stability theory (LST). Flow visualizations and stereoscopic PIV measurements give better insight into the 3D breakdown of the separated shear layer.
When a laminar boundary layer separates because of an adverse streamwise pressure gradient, the flow is subject to increased instability with respect to small-amplitude disturbances. Laminaraturbulent transition occurs under a rapid three-dimensional (3D) development within the separated shear layer. When the following turbulent boundary layer reattaches, a laminar separation bubble is formed. To allow controlled measurements, a small-amplitude TollmienaSchlichting wave (TS wave) was introduced into the boundary layer without (case I) and with (case II) spanwise forcing of steady 3D disturbances. Combined application of laser-Doppler anemometry (LDA) and particle image velocimetry (PIV) demonstrates the suitability of both measurement techniques to capture the development of unsteady, periodic phenomena. The transition mechanism occurring in the flow field under consideration is discussed, and results obtained by controlled measurements are compared to direct numerical simulations (DNS) and predictions from linear stability theory (LST). Flow visualizations and stereoscopic PIV measurements give better insight into the 3D breakdown of the separated shear layer.
Author Lang, M.
Rist, U.
Wagner, S.
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Issue 1
Keywords Vortex shedding
Test facilities
Stereoscopy
Separation bubble
Laser Doppler anemometers
Control systems
Particle image velocimetry
Transition flow
Experimental study
Velocity measurement
Turbulent laminar transition
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StartPage 43
SubjectTerms Bubbles
Disturbances
Exact sciences and technology
Fluid dynamics
Fundamental areas of phenomenology (including applications)
Instability
Instrumentation for fluid dynamics
Laminar
Physics
Separation
Shear layers
Stability
Three dimensional
Transition to turbulence
Turbulence control
Turbulent flows, convection, and heat transfer
Title Investigations on controlled transition development in a laminar separation bubble by means of LDA and PIV
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