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

Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S. / MICROFICHE COPY ALSO AVAILABLE IN AERO LIBRARY. / Bibliography: leaf 94. / M.S.

Identiferoai:union.ndltd.org:MIT/oai:dspace.mit.edu:1721.1/13550
Date January 1970
CreatorsMandell, Gordon Keith
ContributorsTheodore H.H. Pian., Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics
PublisherMassachusetts Institute of Technology
Source SetsM.I.T. Theses and Dissertation
LanguageEnglish
Detected LanguageEnglish
TypeThesis
Formatix, 97 leaves, 5476185 bytes, 5475942 bytes, application/pdf, application/pdf, application/pdf
RightsM.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

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