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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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