Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft
Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, February 2014.
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| Format: | Thesis |
| Language: | eng |
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Massachusetts Institute of Technology
2014
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| Online Access: | http://hdl.handle.net/1721.1/87483 |
| _version_ | 1811071355743895552 |
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| author | Espitia, Alejandro E |
| author2 | Edward M. Greitzer. |
| author_facet | Edward M. Greitzer. Espitia, Alejandro E |
| author_sort | Espitia, Alejandro E |
| collection | MIT |
| description | Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, February 2014. |
| first_indexed | 2024-09-23T08:49:55Z |
| format | Thesis |
| id | mit-1721.1/87483 |
| institution | Massachusetts Institute of Technology |
| language | eng |
| last_indexed | 2024-09-23T08:49:55Z |
| publishDate | 2014 |
| publisher | Massachusetts Institute of Technology |
| record_format | dspace |
| spelling | mit-1721.1/874832019-04-10T19:15:33Z Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft Espitia, Alejandro E Edward M. Greitzer. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Massachusetts Institute of Technology. Department of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis: S.M., Massachusetts Institute of Technology, Department of Aeronautics and Astronautics, February 2014. Cataloged from PDF version of thesis. "September 2013." Page [80] blank. Includes bibliographical references (pages 77-79). Simulations are presented for 1:20 and 1:11 scale configurations of an advanced civil transport designed to use boundary layer ingestion (BLI). Comparison with wind tunnel results on unpowered configurations show that the computed and measured lift slopes agree within 15% and the drag at simulated cruise point to within 20%. Computations have been carried out for an initial and a redesigned configuration of the aft section of the aircraft. The redesigned version showed a reduction in lift and an increase in drag compared to the initial design. The mechanical power for a 1:11 powered configuration at cruise, without BLI, has also been calculated. by Alejandro E. Espitia. S.M. 2014-05-23T19:36:30Z 2014-05-23T19:36:30Z 2013 2014 Thesis http://hdl.handle.net/1721.1/87483 879663610 eng M.I.T. theses are protected by copyright. They may be viewed from this source for any purpose, but reproduction or distribution in any format is prohibited without written permission. See provided URL for inquiries about permission. http://dspace.mit.edu/handle/1721.1/7582 79, 1 unnumbered pages application/pdf Massachusetts Institute of Technology |
| spellingShingle | Aeronautics and Astronautics. Espitia, Alejandro E Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft |
| title | Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft |
| title_full | Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft |
| title_fullStr | Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft |
| title_full_unstemmed | Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft |
| title_short | Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft |
| title_sort | application of overset grids for aerodynamic assessment of an advanced civil transport aircraft |
| topic | Aeronautics and Astronautics. |
| url | http://hdl.handle.net/1721.1/87483 |
| work_keys_str_mv | AT espitiaalejandroe applicationofoversetgridsforaerodynamicassessmentofanadvancedciviltransportaircraft |