2008
DOI: 10.1016/j.cryogenics.2008.03.006
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Integrated numerical prediction of atomization process of liquid hydrogen jet

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Cited by 30 publications
(10 citation statements)
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“…A large body of work in the open literature involves measurements and modeling of spray nozzle internal and external flows (Arcoumanis and Gavaises, 1998;Chen et al, 1998;Founti et al, 2007;Menard et al, 2007;Ishimoto et al, 2008;Som and Aggarwal, 2008;Strasser, 2008;Collazo et al, 2009;Fu et al, 2009). In general, many authors show a SMD / L C We Àx relation, where ''x'' ranges from 0.33 to 0.8, SMD is the Sauter mean droplet diameter, We is the Weber number (qU 2 L c /r), and L c is some characteristic length scale, often taken as the outer diameter D O shown in Fig.…”
Section: Atomizationmentioning
confidence: 99%
“…A large body of work in the open literature involves measurements and modeling of spray nozzle internal and external flows (Arcoumanis and Gavaises, 1998;Chen et al, 1998;Founti et al, 2007;Menard et al, 2007;Ishimoto et al, 2008;Som and Aggarwal, 2008;Strasser, 2008;Collazo et al, 2009;Fu et al, 2009). In general, many authors show a SMD / L C We Àx relation, where ''x'' ranges from 0.33 to 0.8, SMD is the Sauter mean droplet diameter, We is the Weber number (qU 2 L c /r), and L c is some characteristic length scale, often taken as the outer diameter D O shown in Fig.…”
Section: Atomizationmentioning
confidence: 99%
“…Sussman and Puckett carried out the simulation of the jet breakup in Rayleigh mode using a coupled level‐set‐VOF approach. Ishimoto investigated a 3‐D structure of the liquid atomisation behaviour of an LH2 jet flow through a pinhole nozzle based on the LES‐VOF model in conjunction with the CSF model. These analysis focus on the thermodynamic effect on the consecutive breakup of a cryogenic liquid column, and the formation of a liquid film.…”
Section: Introductionmentioning
confidence: 99%
“…The numerical simulation of a SN 2 particle and surrounding gaseous nitrogen (GN 2 ) flow composed of two immiscible fluids involves a combination of three tasks: 1) resolving the flow field, 2) updating the position of the interface and 3) resolving the cryogenic thermal field. The first task is completed by solving the Navier-Stokes equations taking into account the effect of the subgrid scale atomizing flow field by LES [8,9,10]. The second task is performed using the Volume of Fluid (VOF) method [11,12,13].…”
Section: Computational Study For Cooling Heat Transfer and Impingemenmentioning
confidence: 99%