1998
DOI: 10.1615/atomizspr.v8.i4.60
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Diesel Spray Atomization Model Considering Nozzle Exit Turbulence Conditions

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Cited by 67 publications
(43 citation statements)
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“…The only model we are aware of where tan θ /2 increases with We l0 is that of Skrebkov [5, p. 145], who suggests that (tan θ /2) 2 = Tu 2 0 + 12C ρ g /ρ l − 12/(DWe l0 ) for high Re l0 . The model of Huh et al [12] has no We l0 variation at all. The model of Tsyapko [7] is similar to Huh et al's, except for the addition of a term such that tan θ /2 is linear in Re l0 .…”
Section: Spray Angle θmentioning
confidence: 93%
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“…The only model we are aware of where tan θ /2 increases with We l0 is that of Skrebkov [5, p. 145], who suggests that (tan θ /2) 2 = Tu 2 0 + 12C ρ g /ρ l − 12/(DWe l0 ) for high Re l0 . The model of Huh et al [12] has no We l0 variation at all. The model of Tsyapko [7] is similar to Huh et al's, except for the addition of a term such that tan θ /2 is linear in Re l0 .…”
Section: Spray Angle θmentioning
confidence: 93%
“…In contrast, Skrebkov [5] and Huh et al [12] assume that a representative droplet diameter equals the integral scale Λ multiplied by a constant, avoiding problem 1 but not the others. However, as the integral scale is the largest turbulent scale, this seems plausible for only the largest droplet diameter.…”
Section: Previous Quantitative Theories Of Turbulent Jet Breakupmentioning
confidence: 99%
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“…It is well know that the outlet velocity has significant effects on the fuel spray [11]. Thus, it is necessary to investigate the influence of the fuel temperature on the outlet velocity.…”
Section: Influence On the Outlet Velocitymentioning
confidence: 99%