Inverse asymptotic treatment: capturing discontinuities in fluid flows via equation modification

TL;DR

The paper introduces inverse asymptotic treatment (IAT), a unified framework for capturing discontinuities in fluid flows by modifying governing equations, enabling quick, accurate multi-physics simulations with off-the-shelf numerics.

Contribution

It presents IAT as a novel, equation-level approach to model discontinuities, unifying various methods and simplifying multi-physics flow simulations.

Findings

IAT effectively captures discontinuities in multi-physics fluid flow models.

The approach reduces parameter tuning and improves robustness in compressible flow simulations.

Application to hypersonic flow shows close agreement with advanced CFD solvers.

Abstract

A major challenge in developing accurate and robust numerical solutions to multi-physics problems is to correctly model evolving discontinuities in field quantities, which manifest themselves as interfaces between different phases in multi-phase flows, or as shock and contact discontinuities in compressible flows. When a quick response is required to rapidly emerging challenges, the complexity of bespoke discretization schemes impedes a swift transition from problem formulation to computation, which is exacerbated by the need to compose multiple interacting physics. We introduce "inverse asymptotic treatment" (IAT) as a unified framework for capturing discontinuities in fluid flows that enables building directly computable models based on off-the-shelf numerics. By capturing discontinuities through modifications at the level of the governing equations, IAT can seamlessly handle additional physics and thus enable novice end users to quickly obtain numerical results for various multi-physics scenarios. We outline IAT in the context of phase-field modeling of two-phase incompressible flows, and then demonstrate its generality by showing how localized artificial diffusivity (LAD) methods for single-phase compressible flows can be viewed as instances of IAT. Through the real-world example of a laminar hypersonic compression corner, we illustrate IAT's ability to, within just a few months, generate a directly computable model whose wall metrics predictions for sufficiently small corner angles come close to that of NASA's VULKAN-CFD solver. Finally, we propose a novel LAD approach via "reverse-engineered" PDE modifications, inspired by total variation diminishing (TVD) flux limiters, to eliminate the problem-dependent parameter tuning that plagues traditional LAD. We demonstrate that, when combined with second-order central differencing, it can robustly and accurately model compressible flows.