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Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames

Tonti, Federica (2023) Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames. DLR-Forschungsbericht. DLR-FB-2023-8. Dissertation. RWTH Aachen. doi: 10.57676/ns5k-2t91.

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Item URL in elib:https://elib.dlr.de/196550/
Document Type:Monograph (DLR-Forschungsbericht, Dissertation)
Title:Numerical Modelling of the Acoustic Response of Cryogenic Oxygen-Hydrogen Rocket Flames
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Tonti, FedericaUNSPECIFIEDhttps://orcid.org/0000-0002-2797-349XUNSPECIFIED
Date:2023
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
DOI:10.57676/ns5k-2t91
ISSN:1434-8454
Status:Published
Keywords:combustion instabilities, liquid rocket propellant engines, thermoacoustic instabilities,
Institution:RWTH Aachen
Department:Fakultät für Maschinenwesen
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 - Reusable Space Systems and Propulsion Technology
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Rocket Propulsion Technology
Deposited By: Hanke, Michaela
Deposited On:21 Aug 2023 09:15
Last Modified:21 Aug 2023 09:15

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