| 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 |