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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 (2010) Measurement of Initial Conditions of a Kerosene Spray from a Generic Aeroengine Injector at Elevated Pressure. ISBN 978-80-7399-997-1.

Full text not available from this repository.

Official URL: http://www.ilasseurope2010.org/

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 ad-vanced 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 that performs the on line measurement of the measuring volume was modified to suit the experimental setup. Measurements were performed at 4bar and 10bar. Good mass flux density profiles can be obtained within the lift-off distance of the flame.

Item URL in elib:https://elib.dlr.de/68207/
Document Type:Editorship of Proceedings
Title:Measurement of Initial Conditions of a Kerosene Spray from a Generic Aeroengine Injector at Elevated Pressure
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Freitag, StefanATUNSPECIFIED
Ulrich, MeierATUNSPECIFIED
Johannes, HeinzeATUNSPECIFIED
Thomas, BehrendtATUNSPECIFIED
Christoph, HassaATUNSPECIFIED
Date:6 September 2010
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Editors:
EditorsEmailEditor's ORCID iD
ILASS, _UNSPECIFIEDUNSPECIFIED
ISBN:978-80-7399-997-1
Status:Published
Keywords:aero engine combustor; PDA; elevated air pressure; fuel flux measurements; atomization
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:17 Jan 2011 10:05
Last Modified:16 Aug 2012 13:20

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