# Model reduction for transport-dominated problems via online adaptive bases and adaptive sampling

## TL;DR

This paper introduces an adaptive model reduction method for transport-dominated problems that efficiently captures propagating coherent structures by local basis updates and adaptive sampling, achieving significant runtime speedups.

## Contribution

It proposes a novel adaptive sampling scheme and local basis update strategy tailored for transport-dominated phenomena, improving efficiency over traditional methods.

## Key findings

- Achieves up to tenfold speedup compared to full models.
- Effectively captures wave-type structures with fewer samples.
- Demonstrates applicability on rocket engine combustor model.

## Abstract

This work presents a model reduction approach for problems with coherent structures that propagate over time such as convection-dominated flows and wave-type phenomena. Traditional model reduction methods have difficulties with these transport-dominated problems because propagating coherent structures typically introduce high-dimensional features that require high-dimensional approximation spaces. The approach proposed in this work exploits the locality in space and time of propagating coherent structures to derive efficient reduced models. Full-model solutions are approximated locally in time via local reduced spaces that are adapted with basis updates during time stepping. The basis updates are derived from querying the full model at a few selected spatial coordinates. A core contribution of this work is an adaptive sampling scheme for selecting at which components to query the full model to compute basis updates. The presented analysis shows that, in probability, the more local the coherent structure is in space, the fewer full-model samples are required to adapt the reduced basis with the proposed adaptive sampling scheme. Numerical results on benchmark examples with interacting wave-type structures and time-varying transport speeds and on a model combustor of a single-element rocket engine demonstrate the wide applicability of the proposed approach and runtime speedups of up to one order of magnitude compared to full models and traditional reduced models.