On admissible positions of transonic shocks for steady Euler flows in a 3-D axisymmetric cylindrical nozzle

JOURNAL OF DIFFERENTIAL EQUATIONS

卷:288

Article

Fang, Beixiang^1,2  Gao, Xin³ 

[1] Shanghai Jiao Tong Univ, MOE LSC, Sch Math Sci, Shanghai 200240, Peoples R China

[2] Shanghai Jiao Tong Univ, SHL MAC, Shanghai 200240, Peoples R China

[3] Shanghai Jiao Tong Univ, Sch Math Sci, Shanghai 200240, Peoples R China

关键词: Steady Euler system;    Axisymmetric nozzles;    Transonic shocks;    Receiver pressure;    Existence;   

DOI  :  10.1016/j.jde.2021.04.007

来源: Elsevier

【 摘 要 】

This paper concerns with the existence of transonic shocks for steady Euler flows in a 3-D axisymmetric cylindrical nozzle, which are governed by the Euler equations with the slip boundary condition on the wall of the nozzle and a receiver pressure at the exit. Mathematically, it can be formulated as a free boundary problem with the shock front being the free boundary to be determined. In dealing with the free boundary problem, one of the key points is determining the position of the shock front. To this end, a free boundary problem for the linearized Euler system will be proposed, whose solution gives an initial approximating position of the shock front. Compared with the 2-D case, new difficulties arise due to the additional 0-order terms and singularities along the symmetric axis. New observations and careful analysis will be done to overcome these difficulties. Once the initial approximation is obtained, a nonlinear iteration scheme can be carried out, which converges to a transonic shock solution to the problem. (c) 2021 Elsevier Inc. All rights reserved.

【 授权许可】

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