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20232026
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physics.flu-dyn2026

HiLiftAeroML: High-Fidelity Computational Fluid Dynamics Dataset for High-Lift Aircraft Aerodynamics

Neil Ashton, Adam Clark, Liam Heidt +11

This paper describes the first-ever open-source high-fidelity CFD dataset of a high-lift aircraft for the purpose of AI surrogate model development. The dataset is composed of 1800…

physics.flu-dyn2025

Predictions of flow distortions inside a serpentine diffuser from large-eddy simulations

Rahul Agrawal, Chad Winkler, Sanjeeb Bose +1

This work examines the flow separation and the resulting pressure distortions at the exit plane of a serpentine diffuser operating at both subsonic and transonic conditions. Wallmo…

physics.flu-dyn2024

Non-equilibrium wall model for large eddy simulations of complex flows exhibiting turbulent smooth body separation

Rahul Agrawal, Sanjeeb T. Bose, Parviz Moin

In this work, a non-equilibrium wall model is proposed for the prediction of turbulent flows experiencing adverse pressure gradients, including separated flow regimes. The mean-flo…

physics.flu-dyn2024

Studies of Transonic Aircraft Flows and Prediction of Initial Buffet Onset Using Large-Eddy Simulations

Konrad A. Goc, Rahul Agrawal, Sanjeeb T. Bose +1

This article utilizes the Large-Eddy Simulation (LES) paradigm with a physics-based turbulence modeling approach, including a dynamic subgrid-scale model and an equilibrium wall mo…

physics.flu-dyn2023

Reynolds number dependence of length scales governing turbulent flow separation with application to wall-modeled large-eddy simulations

Rahul Agrawal, Sanjeeb Bose, Parviz Moin

This article proposes a Reynolds number scaling of the required grid points to perform wall-modeled LES of turbulent flows encountering separation off a solid surface. Based on com…

physics.flu-dyn2023

An extension of Thwaites method for turbulent boundary layers

Rahul Agrawal, Sanjeeb T. Bose, Kevin P. Griffin +1

Thwaites (1949) developed an approximate method for determining the evolution of laminar boundary layers. The approximation follows from an assumption that the growth of a laminar…