English

Analysis of variable-step/non-autonomous artificial compression methods

Numerical Analysis 2019-05-01 v2

Abstract

A standard artificial compression (AC) method for incompressible flow is un+1εunεk+un+1εun+1ε+12un+1εun+1ε+pn+1ενΔun+1ε=f ,εpn+1εpnεk+un+1ε=0 \frac{u_{n+1}^{\varepsilon }-u_{n}^{\varepsilon }}{k}+u_{n+1}^{\varepsilon }\cdot \nabla u_{n+1}^{\varepsilon }+{\frac{1}{2}}u_{n+1}^{\varepsilon }\nabla \cdot u_{n+1}^{\varepsilon }+\nabla p_{n+1}^{\varepsilon }-\nu \Delta u_{n+1}^{\varepsilon }=f\text{ ,} \\ \varepsilon \frac{p_{n+1}^{\varepsilon }-p_{n}^{\varepsilon }}{k} +\nabla \cdot u_{n+1}^{\varepsilon }=0 for, typically, ε=k\varepsilon =k (timestep). It is fast, efficient and stable with accuracy O(ε+k)O(\varepsilon +k). For adaptive (and thus variable) timestep knk_{n} (and thus ε=εn\varepsilon =\varepsilon _{n}) its long time stability is unknown. For variable k,εk,\varepsilon this report shows how to adapt a standard AC method to recover a provably stable method. For the associated continuum AC model, we prove convergence of the ε=ε(t)\varepsilon =\varepsilon (t)\ artificial compression model to a weak solution of the incompressible Navier-Stokes equations as ε=ε(t)0\varepsilon =\varepsilon (t)\rightarrow 0. The analysis is based on space-time Strichartz estimates for a non-autonomous acoustic equation. Variable ε,k\varepsilon ,k numerical tests in 2d2d and 3d3d are given for the new AC method.

Cite

@article{arxiv.1809.04650,
  title  = {Analysis of variable-step/non-autonomous artificial compression methods},
  author = {Robin Ming Chen and William Layton and Michael McLaughlin},
  journal= {arXiv preprint arXiv:1809.04650},
  year   = {2019}
}

Comments

22 pages

R2 v1 2026-06-23T04:04:29.915Z