Engine design implications for a blended wing-body aircraft with boundary later ingestion
Name
54069199-MIT.pdf
Description
Full printable version
Size
6.28 MB
Format
Adobe PDF
Checksum (MD5)
c1cc2cf76a72b197d8d9ba332340ced7
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.
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.
Persistent DSpace Link