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This work has received HPC resources from the Dutch national e -infrastructure with the support of SURF Cooperative. J.C. and M.K. acknowledge the support of the European Research Council through Starting Grant No. 803082 GloWing. Moreover, the authors express their gratitude to Dr. A. F. Rius-Vidales, Dr. Giulia Zoppini, and Marina Barahona for fruitful discussions on the topic.

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Franco, Juan AlbertoAuthor

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Article

Streaky perturbations in swept-wing flow over forward-facing step

Publicated to:Physical Review Fluids. 10 (2): 023902- - 2025-02-14 10(2), DOI: 10.1103/PhysRevFluids.10.023902

Authors: Casacuberta, Jordi; Westerbeek, Sven; Franco, Juan Alberto; Groot, Koen J; Hickel, Stefan; Hein, Stefan; Kotsonis, Marios

Affiliations

Delft Univ Technol, Fac Aerosp Engn, Dept Flow Phys & Technol, Kluyverweg 1, NL-2629 HS Delft, Netherlands - Author
German Aerosp Ctr, Inst Aerodynam & Flow Technol, Bunsenstr 10, D-37073 Gottingen, Germany - Author
Univ Politecn Madrid, Plaza Cardenal Cisneros 3, E-28040 Madrid, Spain - Author
Univ Wyoming, Dept Mech Engn, Laramie, WY 82072 USA - Author

Abstract

Stationary velocity-perturbation streaks have recently been identified in laminar sweptwing boundary-layer flow interacting with a surface forward-facing step. Streaky structures at the step promote early laminar-turbulent transition under certain conditions. This work utilizes direct numerical simulations to explore the mechanisms of growth of stationary streaks at the step and provides insight into their origin, nature, and spatial organization. The analysis is mainly focused on, but not restricted to, incoming perturbations in the form of stationary crossflow instability. Stationary streaky structures are found to be universal to swept forward-facing-step flow subjected to three-dimensional perturbations in the incoming boundary layer. The streaks at the step are primarily ascribed to the lift-up effect. They appear as a linear perturbation response of the highly sheared step flow to the cross-stream pattern of incoming perturbations. A mechanism of base-flow deceleration additionally contributes to feeding growth to the streaks. Linear stability analysis carried out through the harmonic Navier-Stokes method confirms that the streaks are a linear perturbation phenomenon. Effects of spanwise perturbation wavelength and effective sweep angle on the mechanisms of the streaks are also assessed.

Keywords

3-dimensional boundary-layerDisturbance growthGortler vorticesInstabilityMechanismNonparallelStabilityTransitionTurbulence

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Bibliometric impact. Analysis of the contribution and dissemination channel

The work has been published in the journal Physical Review Fluids due to its progression and the good impact it has achieved in recent years, according to the agency Scopus (SJR), it has become a reference in its field. In the year of publication of the work, 2025, it was in position , thus managing to position itself as a Q1 (Primer Cuartil), in the category Fluid Flow and Transfer Processes. Notably, the journal is positioned above the 90th percentile.

Leadership analysis of institutional authors

This work has been carried out with international collaboration, specifically with researchers from: Germany; Netherlands; United States of America.