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Numerical Investigation of Combustion Instabilities in a Rocket Combustion Chamber with Supercritical Injection Using a Hybrid RANS/LES Method

Lechtenberg, Ansgar and Gerlinger, Peter (2020) Numerical Investigation of Combustion Instabilities in a Rocket Combustion Chamber with Supercritical Injection Using a Hybrid RANS/LES Method. In: AIAA Scitech 2020 Forum. 58th AIAA Aerospace Sciences Meeting, 06.-10.01.2020, Orlando, USA. doi: 10.2514/6.2020-1162. ISBN 978-162410595-1.

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Official URL: https://arc.aiaa.org/doi/10.2514/6.2020-1162


Item URL in elib:https://elib.dlr.de/134694/
Document Type:Conference or Workshop Item (Speech)
Additional Information:Paper AIAA 2020-1162
Title:Numerical Investigation of Combustion Instabilities in a Rocket Combustion Chamber with Supercritical Injection Using a Hybrid RANS/LES Method
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iD
Lechtenberg, AnsgarUNSPECIFIEDhttps://orcid.org/0000-0003-4745-6921
Gerlinger, PeterUNSPECIFIEDUNSPECIFIED
Date:2020
Journal or Publication Title:AIAA Scitech 2020 Forum
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
DOI :10.2514/6.2020-1162
ISBN:978-162410595-1
Status:Published
Keywords:combustion instability, rocket combustion, supercritical injection
Event Title:58th AIAA Aerospace Sciences Meeting
Event Location:Orlando, USA
Event Type:international Conference
Event Dates:06.-10.01.2020
Organizer:AIAA
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 - ProTAU + Prop2020 Hochleistungstriebwerke (old)
Location: Stuttgart
Institutes and Institutions:Institute of Combustion Technology > Computer Simulation
Deposited By: Geigle, Dr. Klaus Peter
Deposited On:18 Apr 2020 12:12
Last Modified:13 Nov 2020 17:42

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