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Updated: Jul 16, 2025

An Analog Macroscopic Technique for Studying Molecular Hydrodynamic Processes in Dense Gases and Liquids
Published on: December 4, 2017
Adaptive physics-informed neural operator for coarse-grained non-equilibrium flows
Ivan Zanardi1, Simone Venturi1, Marco Panesi2
1Center for Hypersonics and Entry Systems Studies, Department of Aerospace Engineering, University of Illinois Urbana-Champaign, Urbana, 61801, IL, USA.
This study introduces a machine learning (ML) framework to speed up non-equilibrium reacting flow simulations. The hierarchical deep learning model accurately predicts chemical kinetics for hypersonic flight applications.
Area of Science:
- Computational fluid dynamics
- Chemical kinetics
- Machine learning
Background:
- Simulating non-equilibrium reacting flows is computationally intensive.
- Accurate modeling of chemical kinetics is crucial for applications like hypersonic flight.
Purpose of the Study:
- To develop a machine learning (ML)-based surrogate model to enhance computational efficiency in non-equilibrium reacting flow simulations.
- To ensure the ML model adheres to fundamental physical principles.
Main Methods:
- A hierarchical and adaptive deep learning strategy combining dimensionality reduction and neural operators.
- Physics-informed neural operator blocks with soft and hard constraints.
- Transfer learning for simplified training and adaptive prediction for accelerated evaluations.
Main Results:
- Accurate prediction of chemical kinetics for nearly thirty species in 0-D scenarios with a maximum relative error of 4.5%.
- Achieved 1-4.5% accuracy in 1-D shock simulations, with a tenfold speedup over conventional methods.
- Demonstrated adaptive prediction capabilities based on local non-equilibrium conditions.
Conclusions:
- The proposed ML framework provides a foundation for efficient, physics-compliant surrogates for reactive Navier-Stokes solvers.
- Enables accurate characterization of non-equilibrium phenomena in complex multi-dimensional simulations.
- Offers significant speedup for simulating hypersonic flow chemical kinetics.
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