Flow control techniques in a serpentine inlet : an enabling technology to increase the military viability of unmanned air vehicles
Name
54090379-MIT.pdf
Description
Full printable version
Size
22.83 MB
Format
Adobe PDF
Checksum (MD5)
6918fdb7d65ca2b64d75f0b14842b8ec
Author(s)
Luers, Andrew Scott, 1978-
Advisor(s)
James D. Paduano.
Date Issued
2003
Publisher
Massachusetts Institute of Technology
Description
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics; and, (S.M.)--Massachusetts Institute of Technology, Engineering Systems Division, Technology and Policy Program, 2003.
Includes bibliographical references (p. 177-181).
Subjects
Aeronautics and Astronautics.
Technology and Policy Program.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Massachusetts Institute of Technology. Engineering Systems Division
Technology and Policy Program
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
