典型文献
RESEARCH ANNOUNCEMENTS ON"STRUCTURAL STABILITY OF TRANSONIC SHOCK FLOWS WITH EXTERNAL FORCE"
文献摘要：
1 Introduction and Main Results
The studies of transonic shock solutions for inviscid compressible flows in different kinds of nozzles had a long history and had obtained many important new achievements during the past twenty years.Courant and Friedrichs[1]had described the transonic shock phenomena in a de Laval nozzle whose cross section decreases first and then increases.It was observed in experiment that if the upcoming flow becomes supersonic after passing through the throat of the nozzle,to match the prescribed appropriately large exit pressure,a shock front intervenes at some place in the diverging part of the nozzle and the gas is compressed and slowed down to subsonic speed.
文献关键词：
中图分类号：
作者姓名：
WENG Shang-kun;YANG Wen-gang
作者机构：
School of Mathematics and Statistics,Wuhan University,Wuhan 430072,China
文献出处：
引用格式：
[1]WENG Shang-kun;YANG Wen-gang-.RESEARCH ANNOUNCEMENTS ON"STRUCTURAL STABILITY OF TRANSONIC SHOCK FLOWS WITH EXTERNAL FORCE")[J].数学杂志,2022(03):189-192
A类：
ANNOUNCEMENTS,STRUCTURAL,TRANSONIC,EXTERNAL,FORCE,intervenes
B类：
RESEARCH,STABILITY,OF,SHOCK,FLOWS,WITH,Introduction,Main,Results,
The,studies,transonic,shock,solutions,inviscid,compressible,flows,different,kinds,nozzles,had,long,history,obtained,many,important,new,achievements,during,past,twenty,years,Courant,Friedrichs,described,phenomena,Laval,whose,cross,section,decreases,first,then,increases,It,was,observed,experiment,that,upcoming,becomes,supersonic,after,passing,through,throat,match,prescribed,appropriately,large,exit,pressure,front,some,place,diverging,part,gas,compressed,slowed,down,subsonic,speed
AB值：
0.683617
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