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Learning Reduced Fluid Dynamics

AAAI 2024 · Probabilistic and scientific modeling › Dynamical systems · approach: Physics-informed dynamics learning · 1 citations (OpenAlex)

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Learns a low-dimensional, exactly time-reversible reduced model of incompressible inviscid Eulerian fluids by optimizing divergence-free POD-initialized bases on the Grassmannian/Stiefel manifold with stochastic Riemannian optimization against a trajectory-wise discrepancy loss.

Problem

Predicting long-horizon state evolution of ultra high-dimensional, time-reversible fluid dynamic systems is computationally expensive, and existing non-intrusive or PINN-based learned models either are costly or fail to preserve time reversibility and energy.

Approach

Treats the reduced velocity subspace basis as the decision variable, lifts reduced trajectories to the ambient space so they are comparable across bases, proves the trajectory map is differentiable over the Grassmannian under small timesteps, and uses tensor precomputation so the trajectory-wise discrepancy gradient is computed without full-order time integration.

Key results

Measured effects reported in the paper

What was changedWhereMeasuredEffect
Fine-tune POD bases with the proposed trajectory-wise optimizationReduced fluid model · Taylor Vorticesdiscrepancy loss: 87.93%, 90.12%, 91.47%, and 90.16%Helped
Fine-tune POD bases with the proposed trajectory-wise optimizationReduced fluid model · Plume Risediscrepancy loss: 88.82%, 80.94%, 87.60%, and 75.79%Helped
Fine-tune POD bases with the proposed trajectory-wise optimizationReduced fluid model · Plume Rise+Obstaclediscrepancy loss: 92.13%, 81.49%, 85.38%, and 81.70%Helped
Fine-tune POD bases with the proposed trajectory-wise optimizationReduced fluid model · Spherical Plumediscrepancy: 54.65%Helped
Fine-tune POD bases with the proposed trajectory-wise optimizationReduced fluid model · Two Plumediscrepancy: 59.28%Helped
Use full-unrolling rather than one-step training (ablation)Reduced fluid model · Plume Rise, ϵ = 0.05, p = 6discrepancy loss after 3k iterations: 57.39 -> 6.37; 24.12Helped
Use full-unrolling rather than one-step training (ablation)Reduced fluid model · Plume Rise, ϵ = 0.01, p = 9discrepancy loss after 3k iterations: 28.23 -> 5.38; 15.71Helped
Increase the initialization noise level from ˜ϵ = 0.01 to ˜ϵ = 0.5 (ablation)Reduced fluid model on Taylor Vortices · Taylor Vortices, ϵ = 0.05, p = 8initial discrepancy loss: 4.84 -> 22.77Hurt
Increase the initialization noise level from ˜ϵ = 0.01 to ˜ϵ = 0.5 (ablation)Reduced fluid model on Taylor Vortices · Taylor Vortices, ϵ = 0.05, p = 8discrepancy loss after 8k iterations: 0.79 -> 1.51Hurt

Surprising findings

Limitations

Experimental setup

Datasets: simulated trajectories from full-order Eulerian fluid model (Taylor vortices, smoke plume benchmarks)

Benchmarks: Taylor vortices rising smoke plume plume rise with obstacle spherical plume two plumes

Metrics: trajectory-wise discrepancy loss energy conservation runtime

Baselines: POD Dynamic Mode Decomposition PINN-style physics loss one-step training (Brandstetter et al. 2022)

Builds on: Proper Orthogonal Decomposition Galerkin projection reduced-order model (Liu et al. 2015) Pavlov et al. 2011 time-reversible discretization RAMSGrad Physics-informed loss (Sirignano and Spiliopoulos 2018)

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