Projects
Supersonic Intake Multi-Objective Optimisation
Full optimisation framework for arbitrary supersonic intake geometries using Axiomatic Design Theory to decompose conflicting functional requirements, Latin Hypercube sampling with high-fidelity RANS CFD, a Kriging surrogate model, and a Multi-Objective Genetic Algorithm to generate Pareto-optimal configurations trading total pressure recovery against pressure drag. Results form the basis of two AIAA AVIATION 2023 conference papers and Chapter 7 of the textbook Computational Design and Optimization of Supersonic Intakes (Routledge, 2025).
Laminar-to-Turbulent Transition Modelling
Local-correlation-based zero-equation transition model compatible with standard two-equation RANS solvers, encoding transition onset as a function of shape factor, free-stream turbulence intensity, and pressure gradient — with no additional transport equations and negligible solver overhead. A dynamical-systems stability analysis identified spurious fixed points in common intermittency formulations responsible for convergence failures. Validated against flat-plate and turbomachinery test cases and published in Computers & Fluids (2021) and AIAA Journal (2021).
Porous-Medium Passive Flow Control for Transonic SWBLI
Numerical investigation of porous-surface passive control as a method of reducing shock-wave/boundary-layer interaction (SWBLI) losses in transonic regimes. The porous medium enables controlled mass transfer across the interaction region, attenuating the peak adverse pressure gradient and delaying separation without discrete protrusions or moving parts. Published in Shock Waves (2021).
Micro Vortex Generator Design — Ramp and Wedge Types
Systematic evaluation of ramp-type and wedge-type micro vortex generators for boundary-layer re-energisation upstream of high-speed shock-wave/boundary-layer interactions. Introduced a swirl centre tracking post-processing methodology to quantify vortex strength and decay trajectory, enabling systematic comparison across device geometries and operating conditions. A follow-on study characterised tandem arrangements. Published in AIAA Journal 56(9) 2018 and AIAA 2020-2961.
FEST-3D — Open-Source Structured CFD Solver
Lead developer of FEST-3D (Finite-volume Explicit STructured 3-Dimensional solver): a modular, multi-block structured RANS solver supporting MUSCL/WENO reconstruction, explicit Runge-Kutta time integration with local time-stepping, and pluggable turbulence/transition models. Used as the primary in-house solver for the intake optimisation and transition modelling studies above. Published in Journal of Open Source Software 5(46), 2020.