DocumentCode :
2158526
Title :
Transition flow conditions in a cavity formed with an underwater gas ejection
Author :
Kazantseva, E.V.
Author_Institution :
Novosibirsk State Tech. Univ., Russia
fYear :
2002
fDate :
2002
Firstpage :
202
Lastpage :
207
Abstract :
The initial stage of gas emission from a bottom hole into an incompressible liquid is accompanied by the appearance of a gas cavity. At the hole inlet, the gas velocity can be both supersonic and subsonic. Hence, any flow regime, that is, supersonic, subsonic, and transient, are possible theoretically in the cavity itself. An attempt is made to answer the following question: when and under what conditions do flow regimes change?.
Keywords :
Mach number; cavitation; partial differential equations; subsonic flow; supersonic flow; transonic flow; Cauchy problem; bottom hole; conservation laws; gas-liquid interface; incompressible liquid; initial gas emission stage; integral curves; one-dimensional equations; polynomials; relative Mach number; singular solutions; subsonic regime; supersonic flow regime; transition flow conditions; underwater gas ejection cavity; Integral equations;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Science and Technology, 2002. KORUS-2002. Proceedings. The 6th Russian-Korean International Symposium on
Print_ISBN :
0-7803-7427-4
Type :
conf
DOI :
10.1109/KORUS.2002.1027998
Filename :
1027998
Link To Document :
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