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Velocimetry of a LOX jet in a high-pressure combustion field from high-speed flame images

Son, Min and Armbruster, Wolfgang and Martin, Jan (2021) Velocimetry of a LOX jet in a high-pressure combustion field from high-speed flame images. ODAS MOTAR 2021, 2021-06-14, Virtual.

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Item URL in elib:https://elib.dlr.de/145941/
Document Type:Conference or Workshop Item (Speech)
Title:Velocimetry of a LOX jet in a high-pressure combustion field from high-speed flame images
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Son, MinUNSPECIFIEDhttps://orcid.org/0000-0003-3182-0637UNSPECIFIED
Armbruster, WolfgangUNSPECIFIEDhttps://orcid.org/0000-0002-4859-4173UNSPECIFIED
Martin, JanUNSPECIFIEDhttps://orcid.org/0000-0002-5050-2506UNSPECIFIED
Date:2021
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:liquid rocket engine, flame visualization, image correlation velocimetry, multi-variable DMD, combustion instability
Event Title:ODAS MOTAR 2021
Event Location:Virtual
Event Type:international Conference
Event Date:14 June 2021
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project LUMEN (Liquid Upper Stage Demonstrator Engine)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Hanke, Michaela
Deposited On:22 Nov 2021 14:01
Last Modified:24 Apr 2024 20:44

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