Droplets in Turbulence
Interface-resolved simulations of how turbulent eddies stretch, deform and break droplets.
Computational fluid dynamics researcher working on turbulence, multiphase flows and scientific machine learning.
Alex Morgan is a (fictional) research scientist studying turbulent and multiphase flows with high-fidelity simulation and data-driven reduced-order models. This is placeholder text for an academic portfolio template — replace it with your own biography.
Our preprint on operator-inference models for transitional boundary layers is now on arXiv.
I gave an invited talk on wall models for separated flows. Slides are on the talks page.
Delighted to share that our group received a (fictional) three-year grant to continue our work on wall models.
Our study on wall-modelled LES of separated channel flow has been accepted. Congratulations to the whole team!
Two new PhD students joined the group this autumn to work on multiphase flows and scientific machine learning.
Interface-resolved simulations of how turbulent eddies stretch, deform and break droplets.
Making large-eddy simulation affordable for flows that separate, using pressure-gradient-aware wall models.
Neural-network surrogates that respect conservation laws, for fast aerodynamic design sweeps.
Placeholder Journal of Fluid Mechanics, vol. 982, pp. A12
We present a wall-modelled large-eddy simulation framework for separated turbulent channel flow over periodic hills and show that a pressure-gradient-aware switch between equilibrium and non-equilibrium wall models improves reattachment prediction at modest cost. (Placeholder abstract.)
Example Journal of Multiphase Flow, vol. 161, no. 4, pp. 104455
Interface-resolved simulations of droplets in forced turbulence are used to map breakup regimes across Weber and Reynolds numbers. Lorem ipsum dolor sit amet, consectetur adipiscing elit.
Proceedings of the Placeholder Conference on Computational Engineering (PCCE), pp. 211-220
We train physics-informed neural networks on sparse RANS data to predict pressure and skin-friction distributions across a family of airfoils, cutting the cost of design sweeps by two orders of magnitude. Sed do eiusmod tempor incididunt ut labore.