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Measurement of Initial Conditions of a Kerosene Spray from a Generic Aeroengine Injector at Elevated Pressure

Freitag, Stefan and Ulrich, Meier and Johannes, Heinze and Thomas, Behrendt and Christoph, Hassa (2011) Measurement of Initial Conditions of a Kerosene Spray from a Generic Aeroengine Injector at Elevated Pressure. Atomization and Sprays, Volume 21 (Issue 6), pp. 521-535. Begell House. DOI: 10.1615/AtomizSpr.2011003457 ISSN 1044-5110

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Official URL: http://www.begellhouse.com/journals/6a7c7e10642258cc,5ace4bb406841239,0dfe604971a7808f.html

Abstract

Ab initio prediction of aeroengine sprays at realistic conditions is currently not feasible and will remain so for a significant time to come. As a partial solution to the problem, experimental data are generated to validate advanced combustion codes. For that purpose a generic injector was built and operated in an optical single sector combustor. Phase Doppler anemometry and Mie scattering were used. The in-house algorithm for the calculation of volume flux was modified to suit the experimental setup. Measurements were performed at 4 and 10 bars. Good volume flux density results can be obtained within the lift-off distance of the flame.

Item URL in elib:https://elib.dlr.de/74053/
Document Type:Article
Title:Measurement of Initial Conditions of a Kerosene Spray from a Generic Aeroengine Injector at Elevated Pressure
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Freitag, StefanATUNSPECIFIED
Ulrich, MeierATUNSPECIFIED
Johannes, HeinzeATUNSPECIFIED
Thomas, BehrendtATUNSPECIFIED
Christoph, HassaATUNSPECIFIED
Date:2011
Journal or Publication Title:Atomization and Sprays
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Volume:Volume 21
DOI :10.1615/AtomizSpr.2011003457
Page Range:pp. 521-535
Publisher:Begell House
ISSN:1044-5110
Status:Published
Keywords:aeroengine, airblast injector, elevated air pressure, phase Doppler anemometry, fuel flux measurements
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Propulsion Systems (old)
DLR - Research area:Aeronautics
DLR - Program:L ER - Engine Research
DLR - Research theme (Project):L - Combustion Chamber Technologies (old)
Location: Köln-Porz
Institutes and Institutions:Institute of Propulsion Technology > Combustor
Deposited By: Freitag, Stefan
Deposited On:19 Jan 2012 10:54
Last Modified:07 Feb 2013 19:18

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