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dc.contributor.authorSwamy, Yashwanth M.en_US
dc.date.accessioned2012-04-11T21:00:11Z
dc.date.available2012-04-11T21:00:11Z
dc.date.issued2012-04-11
dc.date.submittedJanuary 2011en_US
dc.identifier.otherDISS-11449en_US
dc.identifier.urihttp://hdl.handle.net/10106/9650
dc.description.abstractA new type of turbofan which detonates a fuel-air mixture was theoretically found to perform better than a conventional turbofan. A continuous detonation process is described and considered inside the core of the turbofan. The detonation-type turbofan needs certain modifications to detonate the fuel-air mixture at the core of the turbofan, namely, an annular detonation chamber to achieve continuous detonation. A parametric analysis of the new detonation-type turbofan was developed and used to calculate the performance parameters.en_US
dc.description.sponsorshipLu, Franken_US
dc.language.isoenen_US
dc.publisherAerospace Engineeringen_US
dc.titleParametric Analysis Of A Detonation-type Turbofanen_US
dc.typeM.S.en_US
dc.contributor.committeeChairLu, Franken_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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