TY - GEN
T1 - Anisotropic deep learning transport models for two-dimensional transition-continuum flows
AU - Nair, Ashish S.
AU - Sirignano, Justin A
AU - Singh, Narendra
AU - Panesi, Marco
AU - Macart, Jonathan F.
N1 - This material is based upon work supported by the Department of Defense, Office of Naval Research, under Award Number N00014-22-1-2441. The authors gratefully acknowledge computing resources provided by the Center for Research Computing at the University of Notre Dame.
PY - 2025
Y1 - 2025
N2 - In order to simulate rarefied and non-equilibrium flows accurately, the Boltzmann equations are typically used, but they are computationally expensive and provide only approximate solutions. The Navier-Stokes equations, which are computationally tractable, become unreliable in these regimes due to their reliance on the continuum assumption. To address this, a recent study introduced a deep learning framework that augments the Navier-Stokes equations to accurately predict normal shocks in transition-continuum flow regimes [1, 2]. This framework incorporates known Navier-Stokes physics and ensures consistency with the forward equations, while also applying entropy constraints on the closure model outputs to maintain compliance with the second law of thermodynamics. The deep neural network is trained using adjoint equations, which calculate the loss sensitivities with respect to the dependent variables. Three augmented models and a slip-wall boundary condition model are compared, demonstrating the framework’s effectiveness on two-dimensional shock cases.
AB - In order to simulate rarefied and non-equilibrium flows accurately, the Boltzmann equations are typically used, but they are computationally expensive and provide only approximate solutions. The Navier-Stokes equations, which are computationally tractable, become unreliable in these regimes due to their reliance on the continuum assumption. To address this, a recent study introduced a deep learning framework that augments the Navier-Stokes equations to accurately predict normal shocks in transition-continuum flow regimes [1, 2]. This framework incorporates known Navier-Stokes physics and ensures consistency with the forward equations, while also applying entropy constraints on the closure model outputs to maintain compliance with the second law of thermodynamics. The deep neural network is trained using adjoint equations, which calculate the loss sensitivities with respect to the dependent variables. Three augmented models and a slip-wall boundary condition model are compared, demonstrating the framework’s effectiveness on two-dimensional shock cases.
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U2 - 10.2514/6.2025-1691
DO - 10.2514/6.2025-1691
M3 - Conference contribution
AN - SCOPUS:86000189477
SN - 9781624107238
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
BT - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2025
Y2 - 6 January 2025 through 10 January 2025
ER -