activity
20182024
collaborators

6 papers

math.AP2024

Convergence Rate of the Hypersonic Similarity for Two-Dimensional Steady Potential Flows with Large Data

Gui-Qiang G. Chen, Jie Kuang, Wei Xiang +1

We establish the optimal convergence rate of the hypersonic similarity for two-dimensional steady potential flows with {\it large data} past over a straight wedge in the $BV\cap L^…

math.AP2022

Global well-posedness of shock front solutions to one-dimensional piston problem for combustion Euler flows

Kai Hu, Jie Kuang

This paper is devoted to the well-posedness theory of piston problem for compressible {combustion} Euler flows with physical ignition condition. A significant combustion phenomena…

math.AP2021

Convergence Rate of Hypersonic Similarity for Steady Potential Flows Over Two-Dimensional Lipschitz Wedge

Jie Kuang, Wei Xiang, Yongqian Zhang

This paper is devoted to establishing the convergence rate of the hypersonic similarity for the inviscid steady irrotational Euler flow over a two-dimensional Lipschitz slender wed…

math.AP2020

Stability of transonic contact discontinuity for two-dimensional steady compressible Euler flows in a finitely long nozzle

Feimin Huang, Jie Kuang, Dehua Wang +1

We consider the stability of transonic contact discontinuity for the two-dimensional steady compressible Euler flows in a finitely long nozzle. This is the first work on the mixed-…

math.AP2019

Hypersonic Similarity for the Two Dimensional Steady Potential Flow with Large Data

Jie Kuang, Wei Xiang, Yongqian Zhang

In this paper, we establish the first rigorous mathematical global result on the validation of the hypersonic similarity, which is also called the Mach-number independence principl…

math.AP2018

Stability of supersonic contact discontinuity for two-dimensional steady compressible Euler flows in a finite nozzle

Feimin Huang, Jie Kuang, Dehua Wang +1

In this paper, we study the stability of supersonic contact discontinuity for the two-dimensional steady compressible Euler flows in a finitely long nozzle of varying cross-section…