Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf
Prediction of thermoacoustic instabilities in combustors using linearized Navier-Stokes equations in frequency domain
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Centres, VinnExcellence Center for ECO2 Vehicle design.
KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering. KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Centres, VinnExcellence Center for ECO2 Vehicle design.ORCID iD: 0000-0002-9061-4174
KTH, School of Engineering Sciences (SCI), Centres, Linné Flow Center, FLOW. KTH, School of Engineering Sciences (SCI), Centres, VinnExcellence Center for ECO2 Vehicle design. KTH, School of Engineering Sciences (SCI), Aeronautical and Vehicle Engineering, Marcus Wallenberg Laboratory MWL.ORCID iD: 0000-0003-4103-0129
2015 (English)In: 22nd International Congress on Sound and Vibration, ICSV 2015, International Institute of Acoustics and Vibrations , 2015Conference paper, Published paper (Refereed)
Abstract [en]

The paper presents a numerical methodology for the prediction of the thermoacoustic instabilities with the effects of the mean-flow as well as the viscosity. As an academic standard test case, the configuration within the flame sheet located in the middle of the duct is investigated. First, the ducted flame numerical reference case is solved by the inhomogeneous Helmholtz equations in combination of the n - τ flame model assuming that the flow is at rest. Then, we derive the linearized Navier-Stokes equations (LNSE) in frequency domain in combination of the flame model. The unsteady effect of the flame is modeled by the n - τ flame model in harmonic form, which is essentially a 1D formulation relating the rate of heat release and the acoustic velocity at the reference point.

Place, publisher, year, edition, pages
International Institute of Acoustics and Vibrations , 2015.
Keyword [en]
Acoustic wave velocity, Frequency domain analysis, Linearization, Thermoacoustics, Viscous flow, Academic standards, Frequency domains, Inhomogeneous Helmholtz equations, Linearized navier-stokes equations, Numerical methodologies, Rate of heat release, Thermoacoustic instability, Unsteady effects, Navier Stokes equations
National Category
Mechanical Engineering
Identifiers
URN: urn:nbn:se:kth:diva-194715Scopus ID: 2-s2.0-84971224854ISBN: 9788888942483 (print)OAI: oai:DiVA.org:kth-194715DiVA: diva2:1050022
Conference
22nd International Congress on Sound and Vibration, ICSV 2015, 12 July 2015 through 16 July 2015
Note

Funding Details: FP7-PEOPLE-ITN-2012, EC, European Commission

QC 20161128

Available from: 2016-11-28 Created: 2016-10-31 Last updated: 2016-11-28Bibliographically approved

Open Access in DiVA

No full text

Scopus

Search in DiVA

By author/editor
Na, WeiEfraimsson, GunillaBoij, Susann
By organisation
Aeronautical and Vehicle EngineeringLinné Flow Center, FLOWVinnExcellence Center for ECO2 Vehicle designMarcus Wallenberg Laboratory MWL
Mechanical Engineering

Search outside of DiVA

GoogleGoogle Scholar

Total: 168 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • harvard1
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf