elib
DLR-Header
DLR-Logo -> http://www.dlr.de
DLR Portal Home | Imprint | Privacy Policy | Accessibility | Contact | Deutsch
Fontsize: [-] Text [+]

Multiphysics coupling in the thermoacoustically unstable PRECCINSTA burner described using Doak's Momentum Potential Theory

D'Aniello, Raffaele and Humbert, Sylvain C. and Gövert, Simon and Knobloch, Karsten (2025) Multiphysics coupling in the thermoacoustically unstable PRECCINSTA burner described using Doak's Momentum Potential Theory. Aerospace Science and Technology, 163, p. 110140. Elsevier. doi: 10.1016/j.ast.2025.110140. ISSN 1270-9638.

Full text not available from this repository.

Official URL: https://dx.doi.org/10.1016/j.ast.2025.110140


Item URL in elib:https://elib.dlr.de/214098/
Document Type:Article
Title:Multiphysics coupling in the thermoacoustically unstable PRECCINSTA burner described using Doak's Momentum Potential Theory
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
D'Aniello, RaffaeleUNSPECIFIEDhttps://orcid.org/0000-0003-1601-1356184306392
Humbert, Sylvain C.UNSPECIFIEDhttps://orcid.org/0000-0001-5376-7043UNSPECIFIED
Gövert, SimonUNSPECIFIEDhttps://orcid.org/0000-0003-4593-1776UNSPECIFIED
Knobloch, KarstenUNSPECIFIEDhttps://orcid.org/0000-0002-3424-0809UNSPECIFIED
Date:2025
Journal or Publication Title:Aerospace Science and Technology
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:163
DOI:10.1016/j.ast.2025.110140
Page Range:p. 110140
Publisher:Elsevier
ISSN:1270-9638
Status:Published
Keywords:Momentum Potential Theory (MPT); Thermoacoustic instabilities; PRECCINSTA; Large-Eddy Simulation (LES)
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, L - Future Engines and Engine Integration
Location: Berlin-Charlottenburg
Institutes and Institutions:Institute of Propulsion Technology > Engine Acoustic
Institute of Propulsion Technology > Combustor Simulation
Deposited By: D'Aniello, Raffaele
Deposited On:19 May 2025 08:38
Last Modified:19 May 2025 08:38

Repository Staff Only: item control page

Browse
Search
Help & Contact
Information
OpenAIRE Validator logo electronic library is running on EPrints 3.3.12
Website and database design: Copyright © German Aerospace Center (DLR). All rights reserved.