dc.contributor.author | Behymer, Brady | |
dc.contributor.author | Disque, Brendan | |
dc.contributor.author | Foster, Garett | |
dc.contributor.author | Green, Collin | |
dc.contributor.author | Niles, Jacob | |
dc.contributor.author | Stapp, Blake | |
dc.contributor.author | Thiam, Mouhamed | |
dc.contributor.author | Trenary, Schuyler | |
dc.contributor.author | Valenzuela, Bret | |
dc.contributor.author | Wilson, Jordan | |
dc.date.accessioned | 2018-11-21T21:24:54Z | |
dc.date.available | 2018-11-21T21:24:54Z | |
dc.date.issued | 2018-05-02 | |
dc.identifier | oksd_behymer_HT_2018 | |
dc.identifier.uri | https://hdl.handle.net/11244/302107 | |
dc.description.abstract | This report details the cycle and component design of a gas turbine engine to be used on a 100 passenger supersonic transport. The engine, CE18-Bullet, is a mixed-flow, low-bypass ratio turbofan with a max diameter at the fan of 89 inches and a bypass ratio of 2.1. The fan pressure ratio is 2.5 and core of the engine has a 10-stage compressor, which achieves an overall pressure ratio of 42. The low pressure shaft powers the fan using 2 turbine stages while the high pressure shaft powers the compressor using 2 turbine stages. The advanced design of this engine demonstrates substantial improvements over a previously designed baseline engine in TSFC, thrust, weight, and flight envelope. The CE18-Bullet engine provides an 18.1% improvement of TSFC and a 34.2% improvement on thrust at the cruise condition. | |
dc.format | application/pdf | |
dc.language | en_US | |
dc.rights | Copyright is held by the author who has granted the Oklahoma State University Library the non-exclusive right to share this material in its institutional repository. Contact Digital Library Services at lib-dls@okstate.edu or 405-744-9161 for the permission policy on the use, reproduction or distribution of this material. | |
dc.title | CE18-Bullet: Candidate engine for a next generation supersonic transport | |
osu.filename | oksd_behymer_HT_2018.pdf | |
osu.accesstype | Open Access | |
dc.type.genre | Honors Thesis | |
dc.type.material | Text | |
thesis.degree.discipline | Mechanical and Aerospace Engineering | |
thesis.degree.grantor | Oklahoma State University | |