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Stability of supersonic contact discontinuity for two-dimensional steady compressible Euler flows in a finite nozzle
被引:19
作者:
Huang, Feimin
[1
,2
]
Kuang, Jie
[2
,3
]
Wang, Dehua
[4
]
Xiang, Wei
[5
]
机构:
[1] Hunan Normal Univ, Coll Math & Stat, Changsha 410081, Hunan, Peoples R China
[2] Chinese Acad Sci, Acad Math & Syst Sci, Beijing 100190, Peoples R China
[3] Chinese Acad Sci, Wuhan Inst Phys & Math, Wuhan 430071, Hubei, Peoples R China
[4] Univ Pittsburgh, Dept Math, Pittsburgh, PA 15260 USA
[5] City Univ Hong Kong, Dept Math, Kowloon, Hong Kong, Peoples R China
关键词:
Contact discontinuity;
Supersonic flow;
Free boundary;
Compressible Euler equation;
Finitely long nozzle;
FREE-BOUNDARY PROBLEMS;
TRANSONIC SHOCKS;
LONG NOZZLE;
EXISTENCE;
EQUATIONS;
VACUUM;
SYSTEM;
DUCT;
D O I:
10.1016/j.jde.2018.09.036
中图分类号:
O1 [数学];
学科分类号:
0701 ;
070101 ;
摘要:
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-sections. We formulate the problem as an initial-boundary value problem with the contact discontinuity as a free boundary. To deal with the free boundary value problem, we employ the Lagrangian transformation to straighten the contact discontinuity and then the free boundary value problem becomes a fixed boundary value problem. We develop an iteration scheme and establish some novel estimates of solutions for the first order of hyperbolic equations on a cornered domain. Finally, by using the inverse Lagrangian transformation and under the assumption that the incoming flows and the nozzle walls are smooth perturbations of the background state, we prove that the original free boundary problem admits a unique weak solution which is a small perturbation of the background state and the solution consists of two smooth supersonic flows separated by a smooth contact discontinuity. (C) 2018 Elsevier Inc. All rights reserved.
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页码:4337 / 4376
页数:40
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