2019
DOI: 10.31224/osf.io/k2fnm
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Improving the validation of turbulent jet breakup models

Abstract: Understanding the physics of the breakup of turbulent liquid jets is important for a variety of applications including engine sprays, fire suppression systems, and water jet cutting. Models of turbulent jet breakup allow predictions of quantities of interest like the droplet size distribution and breakup length of the jet. These models are compared against experimental data in a process called validation. If the model predictions are within the experimental uncertainty, then the model is "validated" and believ… Show more

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Cited by 4 publications
(19 citation statements)
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“…Many past researchers believe that breakup in these regimes is caused mainly by ambient gas effects (Dumouchel, 2008;Lin and Reitz, 1998;and Reitz, 1978), but my own analyses cast doubt on these assertions. To be more specific, in the "second wind-induced" (i.e., turbulent surface breakup) regime I find no influence of the ambient gas at all Trettel (2019aTrettel ( , 2020a, which makes the "wind-induced" name seem inappropriate. Sallam (2002, p. 94) agrees with this assessment.…”
Section: Regime Namesmentioning
confidence: 86%
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“…Many past researchers believe that breakup in these regimes is caused mainly by ambient gas effects (Dumouchel, 2008;Lin and Reitz, 1998;and Reitz, 1978), but my own analyses cast doubt on these assertions. To be more specific, in the "second wind-induced" (i.e., turbulent surface breakup) regime I find no influence of the ambient gas at all Trettel (2019aTrettel ( , 2020a, which makes the "wind-induced" name seem inappropriate. Sallam (2002, p. 94) agrees with this assessment.…”
Section: Regime Namesmentioning
confidence: 86%
“…The regressions developed in this work will be presented without discussing how they were obtained. The reader is referred to Trettel (2019aTrettel ( , 2020a to understand the choice of the functional forms. Grant and Middleman (1966, fig.…”
Section: Regimes and Their Physical Mechanismsmentioning
confidence: 99%
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“…(A "plane-averaged" turbulence intensity in this work is defined as Tu 0 ≡ 2k 0 /(3U 2 0 ) where k 0 is a planeaveraged turbulent kinetic energy.) I discuss confounding in detail in another paper at this conference [18]. Essentially, both the turbulence intensity and velocity profile are changing when the nozzle length changes [19].…”
Section: Introductionmentioning
confidence: 99%