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dc.contributor.authorKumar, Rahulen_US
dc.date.accessioned2012-07-25T19:10:22Z
dc.date.available2012-07-25T19:10:22Z
dc.date.issued2012-07-25
dc.date.submittedJanuary 2012en_US
dc.identifier.otherDISS-11658en_US
dc.identifier.urihttp://hdl.handle.net/10106/11122
dc.description.abstractDynamic mode decomposition is applied to study the self-excited fluctuations supported by transversely unstable detonations. The focus of this study is on the effect of forcing on the limit cycle solutions. Using DMD, only the most coherent modes are analyzed. The most coherent modes in this case are the fundamental and the fourth harmonic. The analysis is based on the coherency of the self-excited detonation modes due to turbulence. Analysis reveals coherency is significantly affected with a turbulent Mach number greater than 0.3 and also the regions downstream of the shock are more affected by turbulence than the region just behind the shock. The effect of forcing is also analyzed in terms of the four fundamental energy modes: acoustic, kinetic, entropic and chemical. Results of the modal decomposition suggest that the near shock region is controlled by thermo-acoustic instability and a far field region dominated by convected turbulence.en_US
dc.description.sponsorshipMassa, Lucaen_US
dc.language.isoenen_US
dc.publisherAerospace Engineeringen_US
dc.titleDynamic Mode Decomposition Of Detonation Wavesen_US
dc.typeM.S.en_US
dc.contributor.committeeChairMassa, Lucaen_US
dc.degree.departmentAerospace Engineeringen_US
dc.degree.disciplineAerospace Engineeringen_US
dc.degree.grantorUniversity of Texas at Arlingtonen_US
dc.degree.levelmastersen_US
dc.degree.nameM.S.en_US


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