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作 者:WENG Shang-kun YANG Wen-gang
机构地区:[1]School of Mathematics and Statistics,Wuhan University,Wuhan 430072,China
出 处:《数学杂志》2022年第3期189-192,共4页Journal of Mathematics
基 金:Supported By National Natural Science Foundation(11701431,11971307,12071359)。
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 phenomenain a de Laval nozzle whose cross section decreases first and then increases.
关 键 词:shock COMPRESSIBLE FLOWS
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