Data-driven nonlinear aerodynamics models with certifiably optimal boundedness properties

TL;DR

This paper introduces a data-driven method that guarantees bounded long-term predictions for aerodynamic flow models by integrating recent theoretical advances with convex optimization, demonstrated on challenging low-order flow problems.

Contribution

It develops a convex semi-definite programming approach to certify and compute globally attracting bounded models within the SINDy framework for fluid dynamics.

Findings

Successfully applied to benchmark problems demonstrating bounded predictions.

Accurately modeled unsteady separation over an airfoil at high Reynolds number.

Ensured indefinite boundedness of flow predictions in complex nonlinear flows.

Abstract

Obtaining predictive low-order models is a central challenge in fluid dynamics. Data-driven frameworks have been widely used to obtain low-order models of aerodynamic systems; yet, resulting models tend to yield predictions that grow unbounded with time. Recently introduced stability-promoting methods can facilitate the identification of bounded models, but tend to require extensive brute-force tuning even in the context of simple academic systems. Here, we show how recent theoretical advances in the long-term boundedness of dynamical systems can be integrated into data-driven modeling frameworks to ensure that resulting models will yield bounded predictions of incompressible flows. Specifically, we propose to solve a specific set of convex semi-definite programming problems to (i) certify whether a system admits a globally attracting bounded set for the chosen modeling parameters, and (ii) compute a model with the optimal (tightest) bound on this globally attracting set. We demonstrate the approach via integration within the sparse identification of nonlinear dynamics (SINDy) modeling framework. Application on two low-order benchmark problems establishes the merits of the approach. We then apply our approach to obtain a low-order (6-mode) model of unsteady separation over a NACA-65(1)-412 airfoil at Re = 20, 0000, a flow that has been notoriously difficult to model using data-driven methods. The resulting model is found to accurately predict the dynamics of unsteady separation, with model predictions remaining bounded indefinitely. We anticipate this work will benefit future efforts in modeling strongly nonlinear flows, especially in settings where physically-viable long-term forecasts are paramount.