Wall-cooling for transition delay in crossflow-dominated boundary layers

This work will present results where the application of TSP is used to investigate thermal flow control. The focus will be on studying the impact of wall cooling in laminar-to-turbulent transition driven by stationary crossflow instabilities (S-CFI). For that purpose, a detailed parametric study is conducted, varying the cooling temperature ratio and DRE forcing parameters (amplitude and wavelength), with TSP measurements used to obtain accurate transition front location. Complementary HWA measurements, employing a V-wire probe configuration, will also be presented. The combined use of two-component HWA and TSP provides a comprehensive experimental dataset, enabling precise identification of the transition front and detailed analysis of both steady and unsteady perturbations in the streamwise (u) and spanwise (w) velocity components.

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Publication Details

Journal
elib (German Aerospace Center)
Published
2025-11-04
Primary Topic
Fluid Dynamics and Turbulent Flows
Type
article
Field-Weighted Citation Impact
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article

Wall-cooling for transition delay in crossflow-dominated boundary layers

Alberto F. Rius-Vidales, Marco Costantini, Marios Kotsonis, Marina Barahona Lopez
elib (German Aerospace Center)
Fluid Dynamics and Turbulent Flows
article

Wall-cooling for transition delay in crossflow-dominated boundary layers

Alberto F. Rius-Vidales, Marco Costantini, Marios Kotsonis, Marina Barahona Lopez
article en

Abstract

This work will present results where the application of TSP is used to investigate thermal flow control. The focus will be on studying the impact of wall cooling in laminar-to-turbulent transition driven by stationary crossflow instabilities (S-CFI). For that purpose, a detailed parametric study is conducted, varying the cooling temperature ratio and DRE forcing parameters (amplitude and wavelength), with TSP measurements used to obtain accurate transition front location. Complementary HWA measurements, employing a V-wire probe configuration, will also be presented. The combined use of two-component HWA and TSP provides a comprehensive experimental dataset, enabling precise identification of the transition front and detailed analysis of both steady and unsteady perturbations in the streamwise (u) and spanwise (w) velocity components.

elib (German Aerospace Center)
Technische Universiteit Delft
Openalex Percentile: Top 32%
Fluid Dynamics and Turbulent Flows
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