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Parametric Analysis Of A Detonation-type Turbofan

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Parametric Analysis Of A Detonation-type Turbofan

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dc.contributor.author Swamy, Yashwanth M. en_US
dc.date.accessioned 2012-04-11T21:00:11Z
dc.date.available 2012-04-11T21:00:11Z
dc.date.issued 2012-04-11
dc.date.submitted January 2011 en_US
dc.identifier.other DISS-11449 en_US
dc.identifier.uri http://hdl.handle.net/10106/9650
dc.description.abstract A 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.sponsorship Lu, Frank en_US
dc.language.iso en en_US
dc.publisher Aerospace Engineering en_US
dc.title Parametric Analysis Of A Detonation-type Turbofan en_US
dc.type M.S. en_US
dc.contributor.committeeChair Lu, Frank en_US
dc.degree.department Aerospace Engineering en_US
dc.degree.discipline Aerospace Engineering en_US
dc.degree.grantor University of Texas at Arlington en_US
dc.degree.level masters en_US
dc.degree.name M.S. en_US

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