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Swirl-Nozzle Interaction Experiments: Influence of Injection-Reservoir Pressure and Injection Time.

Hirschberg, Lionel and Bake, Friedrich and Knobloch, Karsten and Hulshoff, Steven J. (2021) Swirl-Nozzle Interaction Experiments: Influence of Injection-Reservoir Pressure and Injection Time. AIAA Journal, 59 (7), pp. 2806-2810. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.J060291. ISSN 0001-1452.

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Official URL: https://arc.aiaa.org/toc/aiaaj/59/7


Item URL in elib:https://elib.dlr.de/147965/
Document Type:Article
Title:Swirl-Nozzle Interaction Experiments: Influence of Injection-Reservoir Pressure and Injection Time.
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hirschberg, LionelUNSPECIFIEDhttps://orcid.org/0000-0002-2732-6639UNSPECIFIED
Bake, FriedrichUNSPECIFIEDhttps://orcid.org/0000-0002-3235-428XUNSPECIFIED
Knobloch, KarstenUNSPECIFIEDhttps://orcid.org/0000-0002-3424-0809UNSPECIFIED
Hulshoff, Steven J.UNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:14 May 2021
Journal or Publication Title:AIAA Journal
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:59
DOI:10.2514/1.J060291
Page Range:pp. 2806-2810
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
Series Name:Technical Notes
ISSN:0001-1452
Status:Published
Keywords:Vortex Noise, indirect combustion noise, experimental investigation
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Aeronautics
HGF - Program Themes:Clean Propulsion
DLR - Research area:Aeronautics
DLR - Program:L CP - Clean Propulsion
DLR - Research theme (Project):L - Components and Emissions
Location: Berlin-Charlottenburg
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Deposited By: Knobloch, Dr. Karsten
Deposited On:10 Jan 2022 09:24
Last Modified:10 Jan 2022 09:24

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