The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

In this paper we study the impact of density ratio on the liquid jet in crossflow penetration, deformation, and atomization if all other characteristic parameters, i.e. momentum flux ratio, jet and crossflow Weber and Reynolds numbers, are maintained constant. We perform detailed simulations of the primary atomization region using the refined level set grid method to track the motion of the liquid/gas phase interface. We employ a balanced force, interface projected curvature method to ensure high accuracy of the surface tension forces, use a multi-scale approach to transfer broken off, small scale nearly spherical drops into a Lagrangian point particle description allowing for full two-way coupling and continued secondary atomization, and employ a dynamic Smagorinsky large eddy simulation approach in the single phase regions of the flow to describe turbulence. We compare simulation results obtained previously using a liquid to gas density ratio of 10 for a momentum flux ratio 6.6, Weber number 330, and Reynolds number 14000 liquid jet injected into a Reynolds number 740,000 gaseous crossflow to those at a density ratio of 100, a value typical for gas turbine combustors. The results show that the increase in density ratio results in a noticeable increase in jet penetration and decrease in liquid core deformation in the transverse direction.

Original languageEnglish (US)
Title of host publicationWestern States Section of the Combustion Institute Spring Technical Meeting 2010
PublisherWestern States Section/Combustion Institute
Pages191-205
Number of pages15
ISBN (Print)9781617384196
StatePublished - 2010
EventWestern States Section of the Combustion Institute Spring Technical Meeting 2010 - Boulder, United States
Duration: Mar 22 2010Mar 23 2010

Other

OtherWestern States Section of the Combustion Institute Spring Technical Meeting 2010
CountryUnited States
CityBoulder
Period3/22/103/23/10

Fingerprint

atomizing
Atomization
Liquids
liquids
Reynolds number
Momentum
penetration
Fluxes
momentum
Phase interfaces
Density of gases
gas turbines
Large eddy simulation
gas density
large eddy simulation
combustion chambers
Combustors
Gas turbines
Surface tension
interfacial tension

ASJC Scopus subject areas

  • Chemical Engineering(all)
  • Physical and Theoretical Chemistry
  • Mechanical Engineering

Cite this

Herrmann, M. (2010). The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow. In Western States Section of the Combustion Institute Spring Technical Meeting 2010 (pp. 191-205). Western States Section/Combustion Institute.

The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow. / Herrmann, Marcus.

Western States Section of the Combustion Institute Spring Technical Meeting 2010. Western States Section/Combustion Institute, 2010. p. 191-205.

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Herrmann, M 2010, The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow. in Western States Section of the Combustion Institute Spring Technical Meeting 2010. Western States Section/Combustion Institute, pp. 191-205, Western States Section of the Combustion Institute Spring Technical Meeting 2010, Boulder, United States, 3/22/10.
Herrmann M. The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow. In Western States Section of the Combustion Institute Spring Technical Meeting 2010. Western States Section/Combustion Institute. 2010. p. 191-205
Herrmann, Marcus. / The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow. Western States Section of the Combustion Institute Spring Technical Meeting 2010. Western States Section/Combustion Institute, 2010. pp. 191-205
@inproceedings{8585142fea004b8caca3dce5cceb7d49,
title = "The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow",
abstract = "In this paper we study the impact of density ratio on the liquid jet in crossflow penetration, deformation, and atomization if all other characteristic parameters, i.e. momentum flux ratio, jet and crossflow Weber and Reynolds numbers, are maintained constant. We perform detailed simulations of the primary atomization region using the refined level set grid method to track the motion of the liquid/gas phase interface. We employ a balanced force, interface projected curvature method to ensure high accuracy of the surface tension forces, use a multi-scale approach to transfer broken off, small scale nearly spherical drops into a Lagrangian point particle description allowing for full two-way coupling and continued secondary atomization, and employ a dynamic Smagorinsky large eddy simulation approach in the single phase regions of the flow to describe turbulence. We compare simulation results obtained previously using a liquid to gas density ratio of 10 for a momentum flux ratio 6.6, Weber number 330, and Reynolds number 14000 liquid jet injected into a Reynolds number 740,000 gaseous crossflow to those at a density ratio of 100, a value typical for gas turbine combustors. The results show that the increase in density ratio results in a noticeable increase in jet penetration and decrease in liquid core deformation in the transverse direction.",
author = "Marcus Herrmann",
year = "2010",
language = "English (US)",
isbn = "9781617384196",
pages = "191--205",
booktitle = "Western States Section of the Combustion Institute Spring Technical Meeting 2010",
publisher = "Western States Section/Combustion Institute",

}

TY - GEN

T1 - The influence of density ratio on the primary atomization of a turbulent liquid jet in crossflow

AU - Herrmann, Marcus

PY - 2010

Y1 - 2010

N2 - In this paper we study the impact of density ratio on the liquid jet in crossflow penetration, deformation, and atomization if all other characteristic parameters, i.e. momentum flux ratio, jet and crossflow Weber and Reynolds numbers, are maintained constant. We perform detailed simulations of the primary atomization region using the refined level set grid method to track the motion of the liquid/gas phase interface. We employ a balanced force, interface projected curvature method to ensure high accuracy of the surface tension forces, use a multi-scale approach to transfer broken off, small scale nearly spherical drops into a Lagrangian point particle description allowing for full two-way coupling and continued secondary atomization, and employ a dynamic Smagorinsky large eddy simulation approach in the single phase regions of the flow to describe turbulence. We compare simulation results obtained previously using a liquid to gas density ratio of 10 for a momentum flux ratio 6.6, Weber number 330, and Reynolds number 14000 liquid jet injected into a Reynolds number 740,000 gaseous crossflow to those at a density ratio of 100, a value typical for gas turbine combustors. The results show that the increase in density ratio results in a noticeable increase in jet penetration and decrease in liquid core deformation in the transverse direction.

AB - In this paper we study the impact of density ratio on the liquid jet in crossflow penetration, deformation, and atomization if all other characteristic parameters, i.e. momentum flux ratio, jet and crossflow Weber and Reynolds numbers, are maintained constant. We perform detailed simulations of the primary atomization region using the refined level set grid method to track the motion of the liquid/gas phase interface. We employ a balanced force, interface projected curvature method to ensure high accuracy of the surface tension forces, use a multi-scale approach to transfer broken off, small scale nearly spherical drops into a Lagrangian point particle description allowing for full two-way coupling and continued secondary atomization, and employ a dynamic Smagorinsky large eddy simulation approach in the single phase regions of the flow to describe turbulence. We compare simulation results obtained previously using a liquid to gas density ratio of 10 for a momentum flux ratio 6.6, Weber number 330, and Reynolds number 14000 liquid jet injected into a Reynolds number 740,000 gaseous crossflow to those at a density ratio of 100, a value typical for gas turbine combustors. The results show that the increase in density ratio results in a noticeable increase in jet penetration and decrease in liquid core deformation in the transverse direction.

UR - http://www.scopus.com/inward/record.url?scp=84943419350&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84943419350&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84943419350

SN - 9781617384196

SP - 191

EP - 205

BT - Western States Section of the Combustion Institute Spring Technical Meeting 2010

PB - Western States Section/Combustion Institute

ER -