Advanced Search
DSpace@MIT

Damage tolerance of composite honeycomb sandwich panels under quasi-static bending and cyclic compression

Research and Teaching Output of the MIT Community

Damage tolerance of composite honeycomb sandwich panels under quasi-static bending and cyclic compression

Download
Author: Taylor, Matthew Claire
Other Contributors: Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Advisor: James W. Mar.
Department: Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.
Publisher: Massachusetts Institute of Technology
Date Issued: 1989
Description:
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.Includes bibliographical references (leaves 135-136).
URI: http://hdl.handle.net/1721.1/41237
Keywords: Aeronautics and Astronautics.

Show full item metadata

Files in this item

Name Size Format Description
20834669.pdf 25.80Mb PDF Preview, non-printable (open to all)
20834669-MIT.pdf 25.80Mb PDF Full printable version (MIT only)

This item appears in the following Collection(s)

MIT-Mirage