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Determination of Combustion Response to Acoustic Excitation using High-Speed Visualization

Knapp, Bernhard and Oschwald, Michael (2006) Determination of Combustion Response to Acoustic Excitation using High-Speed Visualization. MOTAR 2006 (Measurement and Observation Techniques for Aerospace Research), 2006-04-06 - 2006-04-07, Berlin.

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Abstract

High frequency measurement of pressure and intensity was performed to indicate pressure or velocity coupling during external excitation. The quantitative analysis of an interaction between an acoustic wave with the processes in combustion chamber (Response Factor) is possible.

Item URL in elib:https://elib.dlr.de/49406/
Document Type:Conference or Workshop Item (Speech)
Title:Determination of Combustion Response to Acoustic Excitation using High-Speed Visualization
Authors:
AuthorsInstitution or Email of AuthorsAuthors ORCID iD
Knapp, BernhardUNSPECIFIEDUNSPECIFIED
Oschwald, MichaelUNSPECIFIEDUNSPECIFIED
Date:7 April 2006
Open Access:No
Gold Open Access:No
In SCOPUS:No
In ISI Web of Science:No
Keywords:combustion instabilities, presure coupling, response factor, external excitation
Event Title:MOTAR 2006 (Measurement and Observation Techniques for Aerospace Research)
Event Location:Berlin
Event Type:international Conference
Event Dates:2006-04-06 - 2006-04-07
Organizer:DLR Berlin
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Space (old)
HGF - Program Themes:W RP - Raumtransport
DLR - Research area:Space
DLR - Program:W RP - Raumtransport
DLR - Research theme (Project):W - Antriebsystemtechnik - Schubkammertechnologie und Hochdruckverbrennung (old)
Location: Lampoldshausen
Institutes and Institutions:Institute of Space Propulsion > Technologie
Deposited By: Knapp, Bernhard
Deposited On:09 Jul 2007
Last Modified:12 Dec 2013 20:25

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