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:

Authors	Institution or Email of Authors	Author's ORCID iD
Lempke, Markus	UNSPECIFIED	UNSPECIFIED
Gerlinger, Peter	UNSPECIFIED	UNSPECIFIED
Aigner, Manfred	UNSPECIFIED	UNSPECIFIED
Seidl, Martin J.	UNSPECIFIED	UNSPECIFIED

Date:

2015

Journal or Publication Title:

Journal of Propulsion and Power

Refereed publication:

Yes

Open Access:

Gold Open Access:

In SCOPUS:

Yes

In ISI Web of Science:

Yes

Volume:

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 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:

13 Nov 2015 10:19

Last Modified:

08 Mar 2018 18:44

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