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Experimental Investigation of Breakup of Turbulent Liquid Jets

Telaar, J. and Schneider, G. and Mayer, W. (2000) Experimental Investigation of Breakup of Turbulent Liquid Jets. In: 16th Annual Conference on Liquid Atomization and Spray Systems, VI.9.1-VI.9.6. ILASS-Europe 2000; 16th Annual Conference on Liquid Atomization and Spray Systems, Darmstadt, 11-13 September 2000.

Full text not available from this repository.

Abstract

This paper summarises recent results of research on the breakup of turbulent liquid jets. In order to investigate the influences of different injection conditions and ambient pressure on the breakup, cold-flow experiments are performed using liquid nitrogen (LN2) at 100 K which is injected into gaseous nitrogen at 300 K. The injection velocities range from 1 to 20 m/s, the ambient pressure from 1 to 6 MPa. The injector diameter is 1.9 mm.

Item URL in elib:https://elib.dlr.de/1485/
Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2000,
Title:Experimental Investigation of Breakup of Turbulent Liquid Jets
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Telaar, J.UNSPECIFIEDUNSPECIFIED
Schneider, G.UNSPECIFIEDUNSPECIFIED
Mayer, W.UNSPECIFIEDUNSPECIFIED
Date:2000
Journal or Publication Title:16th Annual Conference on Liquid Atomization and Spray Systems
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Page Range:VI.9.1-VI.9.6
Editors:
EditorsEmailEditor's ORCID iD
Tropea, C.UNSPECIFIEDUNSPECIFIED
Heukelbach, K., TU-Darmstadt, Germany, UNSPECIFIEDUNSPECIFIED
Status:Published
Event Title:ILASS-Europe 2000; 16th Annual Conference on Liquid Atomization and Spray Systems, Darmstadt, 11-13 September 2000
Organizer:Technische Universität Darmstadt
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):E - no assignment
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Deposited By: Lohmiller, Monika
Deposited On:16 Sep 2005
Last Modified:06 Jan 2010 13:50

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