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  5. Engine design implications for a blended wing-body aircraft with boundary later ingestion

Engine design implications for a blended wing-body aircraft with boundary later ingestion

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Author(s)
Hanlon, Christopher J. (Christopher Joseph), 1978-
Advisor(s)
Charles Boppe and Zoltan S. Spakovszky.
Date Issued
2003
Publisher
Massachusetts Institute of Technology
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2003.
Includes bibliographical references (leaf 91).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Terms of Use
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
Persistent DSpace Link
http://hdl.handle.net/1721.1/82759
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