Non-uniqueness and multi-shock solutions for transonic nozzle flows

被引：0
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作者：
Smith, David H. [1 ]
机构：
[1] 307 EOP, DSTO Edinburgh, P.O. Box 1500, Edinburgh, SA 5111, Australia
来源：
IMA Journal of Applied Mathematics (Institute of Mathematics and Its Applications) | 2006年 / 71卷 / 01期
关键词：
Non-uniqueness for steady inviscid nozzle flows with supersonic inlet and subsonic exit conditions is studied via pseudo-arclength continuation coupled to the discrete flow equations. An interplay between geometry; boundary conditions and bifurcation behaviour is examined; including solutions with one or two shocks. © The Author 2005. Published by Oxford University Press on behalf of the Institute of Mathematics and its Applications. All rights reserved;
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Journal article (JA)
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页码：120 / 132
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