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

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

Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.

Bibliographic Details
Main Author: Taylor, Matthew Claire
Other Authors: James W. Mar.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2008
Subjects:
Aeronautics and Astronautics.
Online Access:http://hdl.handle.net/1721.1/41237

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