TY - GEN
T1 - Physics-constrained deep learning-based model for non-equilibrium flows
AU - Monti, Edoardo
AU - Singh, Narendra
AU - Sirignano, Justin
AU - Macart, Jonathan F.
AU - Panesi, Marco
AU - Gori, Giulio
N1 - Publisher Copyright:
© 2024 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved.
PY - 2024
Y1 - 2024
N2 - In hypersonic applications, the construction of accurate and computationally affordable models for simulating non-equilibrium fluid flows is a challenging task. In particular, designrelevant cases are complex and data availability is poor, de facto hampering the development of constitutive relations of general validity. To circumvent this issue, we propose a methodology for building physics-constrained neural networks providing a correction to the constitutive relation included in the Navier-Stokes model, with a specific focus on rarefied flows. The approach is based on the premise that physical laws should be inherently encoded in robust and accurate closures. By requiring the fulfillment of these laws i.e., by introducing specific constraints to the training process of the neural network, we obtain correction terms coherent with the physics, enhancing the modeling of both the viscous stress tensor and the heat flux vector. The goal is to demonstrate the feasibility of the proposed approach and its potential to benchmark the test case of the 1D shock.
AB - In hypersonic applications, the construction of accurate and computationally affordable models for simulating non-equilibrium fluid flows is a challenging task. In particular, designrelevant cases are complex and data availability is poor, de facto hampering the development of constitutive relations of general validity. To circumvent this issue, we propose a methodology for building physics-constrained neural networks providing a correction to the constitutive relation included in the Navier-Stokes model, with a specific focus on rarefied flows. The approach is based on the premise that physical laws should be inherently encoded in robust and accurate closures. By requiring the fulfillment of these laws i.e., by introducing specific constraints to the training process of the neural network, we obtain correction terms coherent with the physics, enhancing the modeling of both the viscous stress tensor and the heat flux vector. The goal is to demonstrate the feasibility of the proposed approach and its potential to benchmark the test case of the 1D shock.
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U2 - 10.2514/6.2024-0654
DO - 10.2514/6.2024-0654
M3 - Conference contribution
AN - SCOPUS:85192184279
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -