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On Admissible Locations of Transonic Shock Fronts for Steady Euler Flows in an Almost Flat Finite Nozzle with Prescribed Receiver Pressure

  • Published:2020-12-09 Issue:7 Volume:74 Page:1493-1544
  • ISSN:0010-3640
  • Container-title:Communications on Pure and Applied Mathematics
  • language:en
  • Short-container-title:Comm. Pure Appl. Math.

Author:

Fang Beixiang1,Xin Zhouping2

Affiliation:

1. School of Mathematical Sciences MOE‐LSC, and SHL‐MAC, Shanghai Jiao Tong University 800 Dongchuan Road Shanghai 200240 P.R. China

2. The Institute of Mathematical Sciences The Chinese University of Hong Kong Room 701, 7/F, Academic Building No. 1 Shatin N.T. Hong Kong

Publisher

Wiley

Subject

Applied Mathematics,General Mathematics

Cited by 17 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. On uniqueness of steady 1-D shock solutions in a finite nozzle via asymptotic analysis for physical parameters;Journal of Differential Equations;2024-08

2. Smooth Transonic Flows with Nonzero Vorticity to a Quasi Two Dimensional Steady Euler Flow Model;Archive for Rational Mechanics and Analysis;2024-05-22

3. Structural stability of transonic shock flows with an external force;Proceedings of the Royal Society of Edinburgh: Section A Mathematics;2024-04-05

4. Global Stability to Steady Supersonic Rayleigh Flows in One-Dimensional Duct;Chinese Annals of Mathematics, Series B;2024-03

5. Existence of transonic shocks in a cylindrical nozzle with given exit normal momentums;Mathematical Methods in the Applied Sciences;2024-02-15
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