Bayesian optimisation of a roof extension/spoiler on a simplified vehicle, employing wall-resolved LES
File(s)JanczukJFM2026.pdf (3.76 MB)
Accepted version
Author(s)
Janczuk, Kacper
Gaylard, Adrian
Morgans, Aimee
Type
Journal Article
Abstract
A benchmark road vehicle geometry – the squareback Windsor body with wheels and at zero yaw angle – is simulated using high-fidelity Wall-Resolved Large Eddy Simulation (WRLES). Passive control for drag reduction, in the form of optimisation of its rear roof extension, is performed. The rear roof extension is parameterised by its taper penetration distance, angle of incidence and length. This optimisation process uses Gaussian process-based surrogate modelling combined with Bayesian optimisation (Kriging), guided by an expected improvement criterion. The optimisation converged in six iterations (60 simulations), achieving a 6.5% drag reduction. Six distinct drag-reduction mechanisms were identified: diffuser-induced pressure recovery, base size reduction, vertical wake balance modification, separation effects, recirculation region core relocation, and spanwise re-symmetrisation. Rather than isolating individual mechanisms, the study reveals how they interact when multiple geometric parameters are varied concurrently, providing a system-level picture that yields practical design rules. The optimal configuration was found at a roof extension angle of incidence corresponding to the onset of separation, with taper penetration distance and extension length at their maximum values within the analysed domain. These findings establish a robust framework for aerodynamic optimisation and reinforce the effectiveness of
Bayesian optimisation in CFD-based design. In this way, the work bridges fundamental wake studies with applied design practice, showing how coupled wake–geometry interactions can be harnessed for improved aerodynamic performance.
Bayesian optimisation in CFD-based design. In this way, the work bridges fundamental wake studies with applied design practice, showing how coupled wake–geometry interactions can be harnessed for improved aerodynamic performance.
Date Acceptance
2026-01-21
Citation
Journal of Fluid Mechanics
ISSN
0022-1120
Publisher
Cambridge University Press
Journal / Book Title
Journal of Fluid Mechanics
Copyright Statement
Copyright This paper is embargoed until publication. Once published the author’s accepted manuscript will be made available under a CC-BY License in accordance with Imperial’s Research Publications Open Access policy (www.imperial.ac.uk/oa-policy).
License URL
Publication Status
Accepted