Shock formation in solutions to the $2D$ compressible Euler equations in the presence of non-zero vorticity

TL;DR

This paper proves the stability of shock formation in 2D compressible Euler equations with non-zero vorticity, providing a detailed asymptotic description of singularity formation and demonstrating bounded vorticity near shocks.

Contribution

It offers the first constructive analysis of shock formation with non-zero vorticity and no symmetry assumptions, using new geometric and analytic methods.

Findings

Shock formation is stable under perturbations breaking plane symmetry.

Vorticity remains many times differentiable up to the shock in adapted coordinates.

Vorticity remains bounded in Cartesian coordinates up to the shock.

Abstract

We study the Cauchy problem for the compressible Euler equations in two spatial dimensions under any physical barotropic equation of state except that of a Chaplygin gas. We prove that the well-known phenomenon of shock formation in simple plane wave solutions, starting from smooth initial conditions, is stable under perturbations that break the plane symmetry. Moreover, we provide a sharp asymptotic description of the singularity formation. The new feature of our work is that the perturbed solutions are allowed to have small but non-zero vorticity, even at the location of the shock. Thus, our results provide the first constructive description of the vorticity near a singularity formed from compression: relative to a system of geometric coordinates adapted to the acoustic characteristics, the vorticity remains many times differentiable, all the way up to the shock. In addition, relative to the Cartesian coordinates, the vorticity remains bounded up to the shock. To control the vorticity, we rely on a coalition of new geometric and analytic insights that complement the ones used by Christodoulou in his groundbreaking, sharp proof of shock formation in vorticity-free regions. In particular, we rely on a new formulation of the compressible Euler equations exhibiting remarkable structures. To derive estimates, we construct an eikonal function adapted to the acoustic characteristics (which correspond to sound wave propagation) and a related set of geometric coordinates and differential operators. Thanks to the remarkable structure of the equations, the same set of coordinates and differential operators can be used to analyze the vorticity, whose characteristics are transversal to the acoustic characteristics. In particular, our work provides the first constructive description of shock formation without symmetry assumptions in a system with multiple speeds.