Shocks in Quasi-One-Dimensional Bubbly Cavitating Nozzle Flows

2013 ◽  
pp. 205-234
Author(s):  
Can F. Delale ◽  
Günter H. Schnerr ◽  
Şenay Pasinlioğlu
Keyword(s):  
1984 ◽  
Vol 27 (10) ◽  
pp. 2424 ◽  
Author(s):  
N. K. Mitra ◽  
M. Fiebig ◽  
W. Schwan
Keyword(s):  

1999 ◽  
Vol 122 (2) ◽  
pp. 425-430 ◽  
Author(s):  
Yi-Chun Wang

A continuum bubbly mixture model coupled to the Rayleigh-Plesset equation for the bubble dynamics is employed to study one-dimensional steady bubbly cavitating flows through a converging-diverging nozzle. A distribution of nuclei sizes is specified upstream of the nozzle, and the upstream cavitation number and nozzle contraction are chosen so that cavitation occurs in the flow. The computational results show very strong interactions between cavitating bubbles and the flow. The bubble size distribution may have significant effects on the flow; it is shown that it reduces the level of fluctuations and therefore reduces the “cavitation loss” compared to a monodisperse distribution. Another interesting interaction effect is that flashing instability occurs as the flow reaches a critical state downstream of the nozzle. A stability analysis is proposed to predict the critical flow variables. Excellent agreement is obtained between the analytical and numerical results for flows of both equal bubble size and multiple bubble sizes. [S0098-2202(00)00702-1]


Non-equilibrium quasi-one-dimensional nozzle flows are considered in the limit when the relaxation time is large compared with some characteristic flow time. Non-uniformities which arise in the reservoir region, for convergent-divergent nozzles, are treated by the method of matched asymptotic expansions (see, for example, Van Dyke 1964). It is shown that even away from this stagnation zone the solution does not proceed simply in integral powers of the rate parameter. The correct solution is deduced for a vibrationally relaxing gas. It is noted, however, that this near-frozen solution does not necessarily remain valid at downstream infinity where the overall entropy production may become important. Solutions valid in this region are presented in part II of this paper.


The possible existence of compression regions, analogous to condensation shocks, in expanding non-equilibrium nozzle flows is noted. For power-law nozzle shapes the structure and position of these ‘de-excitation shocks’ are derived when the relaxation frequency decays algebraically with temperature. The asymptotic limiting solutions downstream of the de-excitation shocks are also discussed. For certain nozzle shapes it appears that this limiting solution is an infinite sequence of such shocks separated in part by regions of near-frozen flow.


2013 ◽  
Vol 86 (1) ◽  
pp. 49-70 ◽  
Author(s):  
Can F. Delale ◽  
Şenay Pasinlioğlu ◽  
Zafer Başkaya ◽  
Günter H. Schnerr
Keyword(s):  

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