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

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Title: Damage tolerance of composite honeycomb sandwich panels under quasi-static bending and cyclic compression
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
Issue Date: 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.

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