UniFoil: A Universal Dataset of Airfoils in Transitional and Turbulent Regimes for Subsonic and Transonic Flows
Rohit Sunil Kanchi, Benjamin Melanson, Nithin Somasekharan, Shaowu Pan, Sicheng He

TL;DR
UniFoil is a comprehensive, publicly available dataset of over 500,000 airfoil flow simulations covering laminar, transitional, and turbulent regimes across subsonic and transonic flows, designed to advance machine learning in fluid dynamics.
Contribution
It provides the first large-scale, diverse dataset capturing complex flow phenomena including transition and shock interactions for machine learning applications.
Findings
Includes over 4,800 laminar flow airfoils and 30,000 turbulent airfoils.
Supports modeling of laminar-turbulent transition and shock-wave interactions.
Enables development of data-driven models for complex aerodynamic phenomena.
Abstract
We present UniFoil, a large publicly available universal airfoil dataset based on Reynolds-averaged Navier-Stokes (RANS) simulations. It contains over 500,000 samples spanning a wide range of Reynolds and Mach numbers, capturing both transitional and fully turbulent flows across incompressible to compressible regimes. UniFoil is designed to support machine learning research in fluid dynamics, particularly for modeling complex aerodynamic phenomena. Most existing datasets are limited to incompressible, fully turbulent flows with smooth field characteristics, overlooking the critical physics of laminar\-turbulent transition and shock\-wave interactions\-features that exhibit strong nonlinearity and sharp gradients. UniFoil addresses this limitation by offering a broad spectrum of realistic flow conditions. Turbulent simulations utilize the Spalart\-Allmaras (SA) model, while transitional…
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Code & Models
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Taxonomy
TopicsFluid Dynamics and Turbulent Flows · Model Reduction and Neural Networks · Aerodynamics and Acoustics in Jet Flows
