Experimental investigation on flow characteristics of the flash swirl spray

Hyungmin Kim, Woongsup Yoon

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

Abstract

Flow characteristics of atmospheric flash spray from a hollow cone swirl atomizer is experimentally investigated. Velocity fields due to primary and secondary spray formation are optically measured and addressed in conjunction with the drop size distributions. Injectant (water) is pressurized and heated up by controllable line heating system into the thermodynamic state supersaturated in the atmosphere, and exhausted into the atmospheric air by the swirl atomizer. Three dimensional velocity field of the flash swirl spray flow is measured by a multi-plane scanning Stereo-PIV system. The spray flow field is examined in terms of injection pressure and dimensionless superheat degree. The results show that the momentum of the primary and secondary spray is increased simultaneously with increasing in the injection pressure. Formation of the secondary spray heavily depends on the dimensionless superheat degree. The secondary spray grows with the dimensionless superheat degree while the primary spray diminishes.

Original languageEnglish
Title of host publication52nd Aerospace Sciences Meeting
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
ISBN (Electronic)9781624102561
Publication statusPublished - 2014 Jan 1
Event52nd Aerospace Sciences Meeting 2014 - National Harbor, United States
Duration: 2014 Jan 132014 Jan 17

Publication series

Name52nd Aerospace Sciences Meeting

Other

Other52nd Aerospace Sciences Meeting 2014
CountryUnited States
CityNational Harbor
Period14/1/1314/1/17

Fingerprint

Atomizers
Cones
Flow fields
Momentum
Thermodynamics
Scanning
Heating
Air
Water

All Science Journal Classification (ASJC) codes

  • Aerospace Engineering

Cite this

Kim, H., & Yoon, W. (2014). Experimental investigation on flow characteristics of the flash swirl spray. In 52nd Aerospace Sciences Meeting (52nd Aerospace Sciences Meeting). American Institute of Aeronautics and Astronautics Inc..
Kim, Hyungmin ; Yoon, Woongsup. / Experimental investigation on flow characteristics of the flash swirl spray. 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., 2014. (52nd Aerospace Sciences Meeting).
@inproceedings{2d8e9cc3b38d4369be0dfd71226cfebb,
title = "Experimental investigation on flow characteristics of the flash swirl spray",
abstract = "Flow characteristics of atmospheric flash spray from a hollow cone swirl atomizer is experimentally investigated. Velocity fields due to primary and secondary spray formation are optically measured and addressed in conjunction with the drop size distributions. Injectant (water) is pressurized and heated up by controllable line heating system into the thermodynamic state supersaturated in the atmosphere, and exhausted into the atmospheric air by the swirl atomizer. Three dimensional velocity field of the flash swirl spray flow is measured by a multi-plane scanning Stereo-PIV system. The spray flow field is examined in terms of injection pressure and dimensionless superheat degree. The results show that the momentum of the primary and secondary spray is increased simultaneously with increasing in the injection pressure. Formation of the secondary spray heavily depends on the dimensionless superheat degree. The secondary spray grows with the dimensionless superheat degree while the primary spray diminishes.",
author = "Hyungmin Kim and Woongsup Yoon",
year = "2014",
month = "1",
day = "1",
language = "English",
series = "52nd Aerospace Sciences Meeting",
publisher = "American Institute of Aeronautics and Astronautics Inc.",
booktitle = "52nd Aerospace Sciences Meeting",

}

Kim, H & Yoon, W 2014, Experimental investigation on flow characteristics of the flash swirl spray. in 52nd Aerospace Sciences Meeting. 52nd Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics Inc., 52nd Aerospace Sciences Meeting 2014, National Harbor, United States, 14/1/13.

Experimental investigation on flow characteristics of the flash swirl spray. / Kim, Hyungmin; Yoon, Woongsup.

52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc., 2014. (52nd Aerospace Sciences Meeting).

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

TY - GEN

T1 - Experimental investigation on flow characteristics of the flash swirl spray

AU - Kim, Hyungmin

AU - Yoon, Woongsup

PY - 2014/1/1

Y1 - 2014/1/1

N2 - Flow characteristics of atmospheric flash spray from a hollow cone swirl atomizer is experimentally investigated. Velocity fields due to primary and secondary spray formation are optically measured and addressed in conjunction with the drop size distributions. Injectant (water) is pressurized and heated up by controllable line heating system into the thermodynamic state supersaturated in the atmosphere, and exhausted into the atmospheric air by the swirl atomizer. Three dimensional velocity field of the flash swirl spray flow is measured by a multi-plane scanning Stereo-PIV system. The spray flow field is examined in terms of injection pressure and dimensionless superheat degree. The results show that the momentum of the primary and secondary spray is increased simultaneously with increasing in the injection pressure. Formation of the secondary spray heavily depends on the dimensionless superheat degree. The secondary spray grows with the dimensionless superheat degree while the primary spray diminishes.

AB - Flow characteristics of atmospheric flash spray from a hollow cone swirl atomizer is experimentally investigated. Velocity fields due to primary and secondary spray formation are optically measured and addressed in conjunction with the drop size distributions. Injectant (water) is pressurized and heated up by controllable line heating system into the thermodynamic state supersaturated in the atmosphere, and exhausted into the atmospheric air by the swirl atomizer. Three dimensional velocity field of the flash swirl spray flow is measured by a multi-plane scanning Stereo-PIV system. The spray flow field is examined in terms of injection pressure and dimensionless superheat degree. The results show that the momentum of the primary and secondary spray is increased simultaneously with increasing in the injection pressure. Formation of the secondary spray heavily depends on the dimensionless superheat degree. The secondary spray grows with the dimensionless superheat degree while the primary spray diminishes.

UR - http://www.scopus.com/inward/record.url?scp=84938278978&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=84938278978&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:84938278978

T3 - 52nd Aerospace Sciences Meeting

BT - 52nd Aerospace Sciences Meeting

PB - American Institute of Aeronautics and Astronautics Inc.

ER -

Kim H, Yoon W. Experimental investigation on flow characteristics of the flash swirl spray. In 52nd Aerospace Sciences Meeting. American Institute of Aeronautics and Astronautics Inc. 2014. (52nd Aerospace Sciences Meeting).