Global Uniqueness of Transonic Shocks in Divergent Nozzles for Steady Potential Flows
نویسندگان
چکیده
منابع مشابه
Global Uniqueness of Transonic Shocks in Divergent Nozzles for Steady Potential Flows
We show that for steady compressible potential flow in a class of straight divergent nozzles with arbitrary cross-section, if the flow is supersonic and spherically symmetric at the entry, and the given pressure (velocity) is appropriately large (small) and also spherically symmetric at the exit, then there exists uniquely one transonic shock in the nozzle. In addition, the shock-front and the ...
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ژورنال
عنوان ژورنال: SIAM Journal on Mathematical Analysis
سال: 2009
ISSN: 0036-1410,1095-7154
DOI: 10.1137/080740179