Instability and Transition of Swept-Wing Flow: Mechanisms of interaction between crossflow instabilities and forward-facing steps

Research output: ThesisDissertation (TU Delft)

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Abstract

This thesis presents a theoretical and numerical investigation of how a surface forward-facing step alters the stability and transition mechanisms of a laminar incompressible swept-wing boundary layer dominated by stationary crossflow instabilities (CFI). The results elucidate the processes that cause significant transition advancement due to the step and, in turn, challenge the classic paradigm in fluid mechanics that rapid, localised surface-geometry variations are universally detrimental to laminar flow. Through Direct Numerical Simulations (DNS) and new theoretical modelling, this thesis shows that, under specific conditions, a forwardfacing step stabilises pre-existing stationary crossflow vortices and thereby delays laminar-turbulent transition...
Original languageEnglish
QualificationDoctor of Philosophy
Awarding Institution
  • Delft University of Technology
Supervisors/Advisors
  • Kotsonis, M., Promotor
  • Hickel, S., Promotor
Award date11 Dec 2025
Print ISBNs978-94-6384-882-4
DOIs
Publication statusPublished - 2025

Keywords

  • aerodynamics
  • instability
  • transition
  • boundary layer
  • DNS
  • crossflow
  • step
  • flow control

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