DROPLET FORMATION FROM A THIN HOLLOW LIQUID JET WITH A CORE AIR FLOW

2005 ◽  
Vol 15 (5) ◽  
pp. 469-488 ◽  
Author(s):  
Chul Jin Choi ◽  
Sang Yong Lee
2005 ◽  
Vol 15 (4) ◽  
pp. 469-488 ◽  
Author(s):  
Chul Jin Choi ◽  
Sang Yong Lee

1999 ◽  
Vol 9 (4) ◽  
pp. 331-342 ◽  
Author(s):  
Michael P. Moses ◽  
Steven H. Collicott ◽  
Stephen D. Heister

2001 ◽  
Vol 27 (5) ◽  
pp. 636-641
Author(s):  
Yoshio Morozumi ◽  
Jun Fukai ◽  
Osamu Miyatake
Keyword(s):  
Air Flow ◽  

Author(s):  
Tushar Sikroria ◽  
Abhijit Kushari

Abstract This paper presents the experimental analysis of the impact of swirl number of cross-flowing air stream on liquid jet spray trajectory at a fixed air flow velocity of 42 m/s with the corresponding Mach number of 0.12. The experiments were conducted for 4 different swirl numbers (0, 0.2, 0.42 and 0.73) using swirl vanes at air inlet having angles of 0°, 15°, 30° and 45° respectively. Liquid to air momentum flux ratio (q) was varied from 5 to 25. High speed (@ 500 fps) images of the spray were captured and those images were processed using MATLAB to obtain the path of the spray at various momentum flux ratios. The results show interesting trends for the spray trajectory and the jet spread in swirling air flow. High swirling flows not only lead to spray with lower radial penetration due to sharp bending and disintegration of liquid jet, but also result in spray with high jet spread and spray area. Based on the results, correlations for the spray path have been proposed which incorporates the effects of the swirl number of the air flow.


1980 ◽  
Vol 96 (2) ◽  
pp. 275-286 ◽  
Author(s):  
K. C. Chaudhary ◽  
T. Maxworthy

The behaviour of a perturbed capillary jet is experimentally determined by studying the jet from the time it emerges from a small hole to the point at which individual droplets of fluid begin to form. Under any particular set of externally applied experimental parameters, i.e. jet velocity, disturbance wavenumber and amplitude, there is a unique, minimum time to this breakup into drops. This characteristic is needed to relate the magnitude of the input voltage to the modulating device and the output velocity perturbation that it produces. Using this relationship we then compare the experimentally produced profiles of jet shape to corresponding ones calculated by using the theory of Chaudhary & Redekopp (1980). The agreement is satisfactory, especially for small values of input voltage. Then, in the neighbourhood of the cutoff wavenumber, we show that the predicted linear growth of the jet profile is also reproduced in the experimental model.


2001 ◽  
Vol 30 (6) ◽  
pp. 473-484 ◽  
Author(s):  
Takao Inamura ◽  
Takehito Tsutagawa ◽  
Seong Jin Cho ◽  
Goro Masuya

2014 ◽  
Vol 60 ◽  
pp. 103-118 ◽  
Author(s):  
F. Xiao ◽  
M. Dianat ◽  
J.J. McGuirk
Keyword(s):  
Air Flow ◽  

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