2026-09-20T12:30:44Zhttps://dspace.mit.edu/server/oai/requestoai:dspace.mit.edu:1721.1/874832022-01-13T07:53:53Zcom_1721.1_7582com_1721.1_7581col_1721.1_131023
Edward M. Greitzer.
Espitia, Alejandro E
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics.
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
2014-05-23T19:36:30Z
2014-05-23T19:36:30Z
2013
2014
http://hdl.handle.net/1721.1/87483
879663610
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.
79, 1 unnumbered pages
eng
Massachusetts Institute of Technology
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
Aeronautics and Astronautics.
Application of overset grids for aerodynamic assessment of an advanced civil transport aircraft
Thesis
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