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Interpretation of the response of cryogenic rocket flames to forced acoustics using large eddy simulation

Hardi, Justin and Morii, Youhi and Beinke, Scott and Shimizu, Taro and Kawashima, Hideto and Oschwald, Michael (2017) Interpretation of the response of cryogenic rocket flames to forced acoustics using large eddy simulation. In: 31st International Symposium on Space Technology and Science. 31st ISTS, 2017-06-03 - 2017-06-07, Matsuyama, Japan.

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Abstract

Experimental measurement of flame response to acoustics under conditions relevant to industrial engines is challenging and so the scope of such measurements is often limited. High fidelity CFD can be used to model the interaction of acoustic waves with cryogenic flames, and modelling an experimental test case can not only serve as a code validation exercise but also be useful in better characterising the experimental results. This work explores this potential by extending the interpretation of high-speed imaging of representative rocket flames based on comparison with a large eddy simulation of the experiment.

Item URL in elib:https://elib.dlr.de/112847/
Document Type:Conference or Workshop Item (Speech)
Title:Interpretation of the response of cryogenic rocket flames to forced acoustics using large eddy simulation
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Hardi, JustinUNSPECIFIEDhttps://orcid.org/0000-0003-3258-5261UNSPECIFIED
Morii, YouhiJAXA / JEDIUNSPECIFIEDUNSPECIFIED
Beinke, ScottUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Shimizu, TaroJAXA / JEDIUNSPECIFIEDUNSPECIFIED
Kawashima, Hidetojaxa, tsukuba, japanUNSPECIFIEDUNSPECIFIED
Oschwald, MichaelUNSPECIFIEDhttps://orcid.org/0000-0002-9579-9825UNSPECIFIED
Date:6 June 2017
Journal or Publication Title:31st International Symposium on Space Technology and Science
Refereed publication:Yes
Open Access:Yes
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Status:Published
Keywords:rocket engine, cryogenic propellants, combustion instability, optical diagnostics, LES
Event Title:31st ISTS
Event Location:Matsuyama, Japan
Event Type:international Conference
Event Start Date:3 June 2017
Event End Date:7 June 2017
Organizer:JSASS
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):Proj RLV-Schlüsseltechnologien (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion
Institute of Space Propulsion > Rocket Propulsion
Deposited By: Hardi, Dr Justin
Deposited On:26 Jun 2017 08:46
Last Modified:24 Apr 2024 20:17

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