TRANSONIC SHOCK SOLUTIONS TO THE EULER SYSTEM IN DIVERGENT-CONVERGENT NOZZLES

被引:0
|
作者
段犇 [1 ]
兰傲 [2 ]
罗珍 [3 ]
机构
[1] School of Mathematical Sciences,Jilin University
[2] School of Mathematics,Dalian University of Technology
[3] School of Mathematical Sciences,Xiamen University
关键词
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中图分类号
O354 [气体动力学(可压缩流体力学)];
学科分类号
080103 ; 080704 ;
摘要
In this paper,we study the transonic shock solutions to the steady Euler system in a quasi-one-dimensional divergent-convergent nozzle.For a given physical supersonic inflow at the entrance,we obtain exactly two non-isentropic transonic shock solutions for the exit pressure lying in a suitable range.In addition,we establish the monotonicity between the location of the transonic shock and the pressure downstream.
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页码:1536 / 1546
页数:11
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