Damage tolerance of composite honeycomb sandwich panels under quasi-static bending and cyclic compression
Name
20834669-MIT.pdf
Description
Full printable version
Size
25.8 MB
Format
Adobe PDF
Checksum (MD5)
9b46f91b962a1334651f574cc8a94aef
Author(s)
Taylor, Matthew Claire
Advisor(s)
James W. Mar.
Date Issued
1989
Publisher
Massachusetts Institute of Technology
Description
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.
Includes bibliographical references (leaves 135-136).
Subjects
Aeronautics and Astronautics.
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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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.
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