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Unsteady High-Order Simulation of a Liquid Oxygen / Gaseous Hydrogen Rocket Combustor

Lempke, Markus and Gerlinger, Peter and Aigner, Manfred and Seidl, Martin J. (2015) Unsteady High-Order Simulation of a Liquid Oxygen / Gaseous Hydrogen Rocket Combustor. Journal of Propulsion and Power, 31 (6), pp. 1715-1726. American Institute of Aeronautics and Astronautics (AIAA). DOI: 10.2514/1.B35726 ISSN 0748-4658

Full text not available from this repository.

Official URL: http://arc.aiaa.org/doi/pdf/10.2514/1.B35726


Item URL in elib:https://elib.dlr.de/99017/
Document Type:Article
Title:Unsteady High-Order Simulation of a Liquid Oxygen / Gaseous Hydrogen Rocket Combustor
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Lempke, MarkusUNSPECIFIEDUNSPECIFIED
Gerlinger, PeterUNSPECIFIEDUNSPECIFIED
Aigner, ManfredUNSPECIFIEDUNSPECIFIED
Seidl, Martin J.UNSPECIFIEDUNSPECIFIED
Date:2015
Journal or Publication Title:Journal of Propulsion and Power
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:31
DOI :10.2514/1.B35726
Page Range:pp. 1715-1726
Publisher:American Institute of Aeronautics and Astronautics (AIAA)
ISSN:0748-4658
Status:Published
Keywords:rocket combustor, CFD, high order, O2/H2
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transport
DLR - Research area:Raumfahrt
DLR - Program:R RP - Raumtransport
DLR - Research theme (Project):R - ProTAU + Prop2020 Hochleistungstriebwerke
Location: Stuttgart
Institutes and Institutions:Institute of Combustion Technology > Computer Simulation
Deposited By: Geigle, Dr. Klaus Peter
Deposited On:13 Nov 2015 10:19
Last Modified:08 Mar 2018 18:44

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