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Numerical investigation of scramjet strut injector cooling for different fuel mass fluxes and strut material properties at Mach 8 flight conditions

Gerlinger, Peter and Simsont, Yann Hendrik (2019) Numerical investigation of scramjet strut injector cooling for different fuel mass fluxes and strut material properties at Mach 8 flight conditions. Acta Astronautica, 160, pp. 353-364. Elsevier. DOI: 10.1016/j.actaastro.2019.04.042 ISSN 0094-5765

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Official URL: https://doi.org/10.1016/j.actaastro.2019.04.042


Item URL in elib:https://elib.dlr.de/127399/
Document Type:Article
Title:Numerical investigation of scramjet strut injector cooling for different fuel mass fluxes and strut material properties at Mach 8 flight conditions
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Gerlinger, PeterUNSPECIFIEDUNSPECIFIED
Simsont, Yann HendrikUNSPECIFIEDUNSPECIFIED
Date:2019
Journal or Publication Title:Acta Astronautica
Refereed publication:Yes
Open Access:No
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:Yes
Volume:160
DOI :10.1016/j.actaastro.2019.04.042
Page Range:pp. 353-364
Publisher:Elsevier
ISSN:0094-5765
Status:Published
Keywords:Simulation, scramjet, injector cooling, Mach 8 combustor
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 May 2019 07:28
Last Modified:13 May 2019 07:28

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