SPEAKER: Federico Zabaleta, Center for Turbulence Research, Stanford University, Stanford, CA
TOPIC: Large-Eddy Simulations of Conjugate Heat Transfer over Iced Surfaces
WHEN: 9:00 AM PST, Thursday, January 29th, 2026
WHERE: Building N258, Auditorium (Rm. 127), NASA Ames Research Center, Moffett Field, CA
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ABSTRACT
The accurate prediction of aircraft icing remains a critical challenge for flight safety and certification. While various ice accretion codes are currently in use, they frequently exhibit significant uncertainty, particularly in glaze ice conditions. A major contributor to this uncertainty is the lack of high-fidelity heat transfer predictions, which fundamentally govern the local freezing rates and resulting ice morphology. Traditional modeling approaches typically simplify the accretion physics, relying on isothermal wall assumptions and one-dimensional conduction models that fail to capture the complex thermodynamics of realistic ice roughness. This talk presents a high-fidelity, multi-physics framework that integrates wall-modeled large-eddy simulation (WMLES), Lagrangian droplet tracking, and unsteady conjugate heat transfer (CHT) to resolve coupled fluid-solid thermal interactions.

Boundary layer transition over ice-characterized roughness. Iso-surfaces of temperature (T = 299 K) are colored by local velocity magnitude, resolving the interaction between complex surface topology and turbulent flow.
SPEAKER

Federico Zabaleta is a Postdoctoral Fellow at the Center for Turbulence Research (CTR) at Stanford University, where he leads the development of high-fidelity Large Eddy Simulations (LES) for aircraft icing. Working under the direction of Professor Parviz Moin, his research focuses on integrating multi-physics frameworks to improve the predictive accuracy of icing models for safety and certification. Federico holds a BSc in Civil and Hydraulic Engineering from the National University of La Plata, Argentina, and earned both his MSc and PhD from the University of California, Davis. His doctoral research specialized in the development of numerical techniques for simulating air entrainment in complex free-surface flows.
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Jared Duensing Branch Chief Computational Aerosciences Branch (Code TNA) NASA Ames Research Center Mail Stop 258-2 Moffett Field, CA 94035 M: 256.930.1402 |