典型文献
TRANSONIC SHOCK SOLUTIONS TO THE EULER SYSTEM IN DIVERGENT-CONVERGENT NOZZLES
文献摘要：
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.
文献关键词：
中图分类号：
作者姓名：
Ben DUAN;Ao LAN;Zhen LUO
作者机构：
School of Mathematical Sciences,Jilin University,Changchun 130012,China;School of Mathematics,Dalian University of Technology,Dalian 116024,China;School of Mathematical Sciences,Xiamen University,Xiamen 361005,China
文献出处：
引用格式：
[1]Ben DUAN;Ao LAN;Zhen LUO-.TRANSONIC SHOCK SOLUTIONS TO THE EULER SYSTEM IN DIVERGENT-CONVERGENT NOZZLES)[J].数学物理学报（英文版）,2022(04):1536-1546
A类：
TRANSONIC,EULER,DIVERGENT,CONVERGENT,NOZZLES
B类：
SHOCK,SOLUTIONS,TO,THE,SYSTEM,IN,In,this,paper,study,transonic,shock,solutions,steady,Euler,system,quasi,one,dimensional,divergent,convergent,nozzle,For,given,physical,supersonic,inflow,entrance,obtain,exactly,two,isentropic,exit,pressure,lying,suitable,range,addition,establish,monotonicity,between,location,downstream
AB值：
0.630982
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