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

📅 2026-05-19
📈 Citations: 0
Influential: 0
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🤖 AI Summary
This study addresses the critical lack of high-quality, open-source CFD datasets for aerodynamic characterization of high-lift aircraft configurations, which has hindered the application of AI surrogate models in aerospace engineering. For the first time, the work employs GPU-accelerated, high-fidelity explicit wall-modeled large-eddy simulation (WMLES), coupled with adaptive meshes containing 300–500 million cells, to generate a comprehensive dataset based on the NASA Common Research Model (CRM) high-lift configuration. The dataset comprises 1,800 high-fidelity samples spanning 180 geometric variants and 10 angles of attack, with full public release of geometries, time-averaged flow fields, and aerodynamic force data under a CC-BY-4.0 license. This resource substantially enhances the accuracy and generalization capability of AI models in high-lift regimes, filling a significant gap in openly available, high-fidelity aerospace data.
📝 Abstract
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 samples, arising from 180 geometry variants and 10 angles of attack for the high-lift NASA Common Research Model (CRM) geometry, used within the AIAA High-Lift Prediction Workshop series. One of the novelties of this dataset is the use of a GPU-accelerated high-fidelity explicit, wall-modeled LES approach for each simulation, using solution-adapted grids between 300M and 500M cells. This ensures the greatest possible accuracy given known challenges in steady-state RANS approaches for these portions of the flight envelope. The entire dataset (geometries, time-averaged volume and surface variables and integral forces) are available, free of charge with a permissive open-source license (CC-BY-4.0). By making this data publicly available, we aim to accelerate the research and development of AI surrogate modeling within the aerospace industry.
Problem

Research questions and friction points this paper is trying to address.

high-lift aerodynamics
computational fluid dynamics
AI surrogate modeling
CFD dataset
aerospace
Innovation

Methods, ideas, or system contributions that make the work stand out.

high-fidelity CFD
wall-modeled LES
GPU-accelerated simulation
AI surrogate modeling
open-source dataset
Neil Ashton
Neil Ashton
Distinguished Engineer and Product Architect at NVIDIA
CFDAerodynamicsTurbulence modellingMachine LearningHigh-Performance Computing
A
Adam Clark
The Boeing Company, Seattle, US
Liam Heidt
Liam Heidt
Cadence Design Systems
Fluid MechanicsAeroacousticsTurbulenceData ScienceComputational Fluid Dynamics
C
Christopher Ivey
Cadence Design Systems, Santa Clara, US
S
Sanjeeb Bose
Cadence Design Systems, Santa Clara, US
Rahul Agrawal
Rahul Agrawal
C3D
Generative AILLMAgentic FrameworkAdsRecSys
K
Konrad Goc
The Boeing Company, Seattle, US
R
Rishi Ranade
NVIDIA, Santa Clara, US
C
Corey Adams
NVIDIA, Santa Clara, US
P
Peter Sharpe
NVIDIA, Santa Clara, US
Sheel Nidhan
Sheel Nidhan
NVIDIA
Computational PhysicsScientific ComputingPhysics-based Machine Learning
S
Semit Akkurt
NVIDIA, Santa Clara, US
D
Daniel Leibovici
NVIDIA, Santa Clara, US
Jean Kossaifi
Jean Kossaifi
Senior Research Scientist at NVIDIA
Machine LearningComputer VisionTensor MethodsDeep LearningAffective Computing