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  5. Analysis of free-edge effects in composite laminates by an assumed-stress method.

Analysis of free-edge effects in composite laminates by an assumed-stress method.

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Author(s)
Mandell, Gordon Keith
Advisor(s)
Theodore H.H. Pian.
Date Issued
1970
Publisher
Massachusetts Institute of Technology
Description
Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.
MICROFICHE COPY ALSO AVAILABLE IN AERO LIBRARY.
Bibliography: leaf 94.
Subjects
Aeronautics and Astronautics
MIT Department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
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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.
http://dspace.mit.edu/handle/1721.1/7582
Persistent DSpace Link
http://hdl.handle.net/1721.1/13550
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