Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities

Son, Min and Börner, Michael and Armbruster, Wolfgang and Hardi, Justin (2023) Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities. Aerospace. Multidisciplinary Digital Publishing Institute (MDPI). doi: 10.3390/aerospace10050452. ISSN 2226-4310.

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Official URL: https://www.mdpi.com/journal/aerospace

Item URL in elib:

https://elib.dlr.de/200066/

Document Type:

Article

Title:

Orifice Flow Dynamics in a Rocket Injector as an Excitation Source of Injector-Driven Combustion Instabilities

Authors:

Authors	Institution or Email of Authors	Author's ORCID iD	ORCID Put Code
Son, Min	UNSPECIFIED	UNSPECIFIED	UNSPECIFIED
Börner, Michael	UNSPECIFIED	https://orcid.org/0000-0002-3441-2869	147801848
Armbruster, Wolfgang	UNSPECIFIED	https://orcid.org/0000-0002-4859-4173	147801849
Hardi, Justin	UNSPECIFIED	https://orcid.org/0000-0003-3258-5261	UNSPECIFIED

Date:

15 May 2023

Journal or Publication Title:

Aerospace

Refereed publication:

Yes

Open Access:

Yes

Gold Open Access:

Yes

In SCOPUS:

Yes

In ISI Web of Science:

Yes

DOI:

10.3390/aerospace10050452

Publisher:

Multidisciplinary Digital Publishing Institute (MDPI)

ISSN:

2226-4310

Status:

Published

Keywords:

combustion instability; rocket injector; flow visualization; cavitation; whistling

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 - Reusable Space Systems and Propulsion Technology

Location:

Lampoldshausen

Institutes and Institutions:

Institute of Space Propulsion > Rocket Propulsion Technology

Deposited By:

Hanke, Michaela

Deposited On:

30 Nov 2023 15:18

Last Modified:

29 Jan 2024 12:07

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