Surface heating effects on attachment-line transition and relaminarisation
Wall-resolved large-eddy simulations are used to investigate the effects of elevated surface temperature on the leading edge of a swept wing. Earlier stability analyses demonstrate a strong destabilising effect resulting from surface heating, but do not reveal the ultimate effects on transition and relaminarisation. The current results support the findings from stability analysis with elevated surface temperatures, but show a more complex dependency between instability and turbulence than is observed for adiabatic conditions. For attachment-line Reynolds numbers above the adiabatic relaminarisation threshold, instability leads to fully turbulent flow. At Reynolds numbers below the adiabatic relaminarisation threshold, instability leads to finite-amplitude equilibrium states and intermittent turbulent bursting, but not fully turbulent flow.
Authors
- J. D. Crouch (ORCID: https://orcid.org/0000-0003-2375-8781)
- K.A. Goc
Institutions
- Boeing (Australia) (AU)
Publication Details
- Journal
- Journal of Fluid Mechanics
- Published
- 2026-09-11
- DOI
- https://doi.org/10.1017/jfm.2026.11949
- Primary Topic
- Fluid Dynamics and Turbulent Flows
- Type
- article
- Field-Weighted Citation Impact
- 0.00