THE UNIQUENESS OF A TRANSONIC SHOCK IN A NOZZLE FOR THE 2-D COMPLETE EULER SYSTEM WITH THE VARIABLE END PRESSURE

被引:0
|
作者
Dacheng, Cui [1 ]
Huicheng, Yin [1 ]
机构
[1] Nanjing Univ, Dept Math & IMS, Nanjing 210093, Jiangsu, Peoples R China
来源
关键词
Steady Euler system; supersonic flow; subsonic flow; transonic shock; nozzle;
D O I
暂无
中图分类号
O29 [应用数学];
学科分类号
070104 ;
摘要
In this paper, by use of the methods in [1-3], we establish the uniqueness of a 2-D transonic shock solution in a nozzle when the end pressure in the diverging part of the nozzle lies in an appropriate scope. Especially, we remove the crucial but unnatural assumption in recent references which the transonic shock must be assumed to go through a fixed point in advance.
引用
收藏
页码:263 / 288
页数:26
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