Close Nozzle Spray Characteristics of a Prefilming Airblast Atomizer

The formation of pollutant emissions in jet engines is closely related to the fuel distribution inside the combustor. Hence, the characteristics of the spray formed during primary breakup are of major importance for an accurate prediction of the pollutant emissions. Currently, an Euler−Lag...

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Main Authors: Simon Holz, Samuel Braun, Geoffroy Chaussonnet, Rainer Koch, Hans-Jörg Bauer
Format: Article
Language:English
Published: MDPI AG 2019-07-01
Series:Energies
Subjects:
Online Access:https://www.mdpi.com/1996-1073/12/14/2835
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spelling doaj-9eb9650439fe47998526c67235193a742020-11-25T02:22:45ZengMDPI AGEnergies1996-10732019-07-011214283510.3390/en12142835en12142835Close Nozzle Spray Characteristics of a Prefilming Airblast AtomizerSimon Holz0Samuel Braun1Geoffroy Chaussonnet2Rainer Koch3Hans-Jörg Bauer4Institut für Thermische Strömungsmaschinen, Karlsruher Institut für Technologie, 76131 Karlsruher, GermanySteinbuch Centre for Computing, Karlsruher Institut für Technologie, 76128 Karlsruher, GermanyInstitut für Thermische Strömungsmaschinen, Karlsruher Institut für Technologie, 76131 Karlsruher, GermanyInstitut für Thermische Strömungsmaschinen, Karlsruher Institut für Technologie, 76131 Karlsruher, GermanyInstitut für Thermische Strömungsmaschinen, Karlsruher Institut für Technologie, 76131 Karlsruher, GermanyThe formation of pollutant emissions in jet engines is closely related to the fuel distribution inside the combustor. Hence, the characteristics of the spray formed during primary breakup are of major importance for an accurate prediction of the pollutant emissions. Currently, an Euler−Lagrangian approach for droplet transport in combination with combustion and pollutant formation models is used to predict the pollutant emissions. The missing element for predicting these emissions more accurately is well defined starting conditions for the liquid fuel droplets as they emerge from the fuel nozzle. Recently, it was demonstrated that the primary breakup can be predicted from first principles by the Lagrangian, mesh-free, Smoothed Particle Hydrodynamics (SPH) method. In the present work, 2D Direct Numerical Simulations (DNS) of a planar prefilming airblast atomizer using the SPH method are presented, which capture most of the breakup phenomena known from experiments. Strong links between the ligament breakup and the resulting spray in terms of droplet size, trajectory and velocity are demonstrated. The SPH predictions at elevated pressure conditions resemble quite well the effects observed in experiments. Significant interdependencies between droplet diameter, position and velocity are observed. This encourages to employ such multidimensional interdependence relations as a base for the development of primary atomization models.https://www.mdpi.com/1996-1073/12/14/2835prefilming airblast atomizationprimary breakupligamentspraySmoothed Particle Hydrodynamicsmultivariate statistics
collection DOAJ
language English
format Article
sources DOAJ
author Simon Holz
Samuel Braun
Geoffroy Chaussonnet
Rainer Koch
Hans-Jörg Bauer
spellingShingle Simon Holz
Samuel Braun
Geoffroy Chaussonnet
Rainer Koch
Hans-Jörg Bauer
Close Nozzle Spray Characteristics of a Prefilming Airblast Atomizer
Energies
prefilming airblast atomization
primary breakup
ligament
spray
Smoothed Particle Hydrodynamics
multivariate statistics
author_facet Simon Holz
Samuel Braun
Geoffroy Chaussonnet
Rainer Koch
Hans-Jörg Bauer
author_sort Simon Holz
title Close Nozzle Spray Characteristics of a Prefilming Airblast Atomizer
title_short Close Nozzle Spray Characteristics of a Prefilming Airblast Atomizer
title_full Close Nozzle Spray Characteristics of a Prefilming Airblast Atomizer
title_fullStr Close Nozzle Spray Characteristics of a Prefilming Airblast Atomizer
title_full_unstemmed Close Nozzle Spray Characteristics of a Prefilming Airblast Atomizer
title_sort close nozzle spray characteristics of a prefilming airblast atomizer
publisher MDPI AG
series Energies
issn 1996-1073
publishDate 2019-07-01
description The formation of pollutant emissions in jet engines is closely related to the fuel distribution inside the combustor. Hence, the characteristics of the spray formed during primary breakup are of major importance for an accurate prediction of the pollutant emissions. Currently, an Euler−Lagrangian approach for droplet transport in combination with combustion and pollutant formation models is used to predict the pollutant emissions. The missing element for predicting these emissions more accurately is well defined starting conditions for the liquid fuel droplets as they emerge from the fuel nozzle. Recently, it was demonstrated that the primary breakup can be predicted from first principles by the Lagrangian, mesh-free, Smoothed Particle Hydrodynamics (SPH) method. In the present work, 2D Direct Numerical Simulations (DNS) of a planar prefilming airblast atomizer using the SPH method are presented, which capture most of the breakup phenomena known from experiments. Strong links between the ligament breakup and the resulting spray in terms of droplet size, trajectory and velocity are demonstrated. The SPH predictions at elevated pressure conditions resemble quite well the effects observed in experiments. Significant interdependencies between droplet diameter, position and velocity are observed. This encourages to employ such multidimensional interdependence relations as a base for the development of primary atomization models.
topic prefilming airblast atomization
primary breakup
ligament
spray
Smoothed Particle Hydrodynamics
multivariate statistics
url https://www.mdpi.com/1996-1073/12/14/2835
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