Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor

Gröning, Stefan and Hardi, Justin and Suslov, Dmitry and Oschwald, Michael (2016) Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor. Journal of Propulsion and Power. American Institute of Aeronautics and Astronautics (AIAA). doi: 10.2514/1.B35768. ISSN 0748-4658.

Full text not available from this repository.

Item URL in elib:

https://elib.dlr.de/107792/

Document Type:

Article

Title:

Injector-Driven Combustion Instabilities in a Hydrogen/Oxygen Rocket Combustor

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Gröning, Stefan	Institut für Raumfahrtantriebe, DLR Lampoldshausen	UNSPECIFIED	UNSPECIFIED
Hardi, Justin	UNSPECIFIED	https://orcid.org/0000-0003-3258-5261	UNSPECIFIED
Suslov, Dmitry	UNSPECIFIED	https://orcid.org/0000-0002-5160-9292	UNSPECIFIED
Oschwald, Michael	UNSPECIFIED	https://orcid.org/0000-0002-9579-9825	UNSPECIFIED

Date:

2016

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

DOI:

10.2514/1.B35768

Publisher:

American Institute of Aeronautics and Astronautics (AIAA)

ISSN:

0748-4658

Status:

Published

Keywords:

high frequency combustion, rocket propulsion

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 - Antriebsystemtechnik - Schubkammertechnologie (old)

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Rocket Propulsion

Deposited By:

Hanke, Michaela

Deposited On:

16 Nov 2016 07:50

Last Modified:

27 Nov 2023 14:00

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