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.

Bibliographic Details
Main Author: Mandell, Gordon Keith
Other Authors: Theodore H.H. Pian.
Format: Thesis
Language:eng
Published: Massachusetts Institute of Technology 2005
Subjects:
Online Access:http://hdl.handle.net/1721.1/13550
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author Mandell, Gordon Keith
author2 Theodore H.H. Pian.
author_facet Theodore H.H. Pian.
Mandell, Gordon Keith
author_sort Mandell, Gordon Keith
collection MIT
description Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Thesis. 1970. M.S.
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spelling mit-1721.1/135502019-04-12T21:16:24Z Analysis of free-edge effects in composite laminates by an assumed-stress method. Mandell, Gordon Keith Theodore H.H. Pian. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics Aeronautics and Astronautics 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. 2005-08-10T21:55:45Z 2005-08-10T21:55:45Z 1970 Thesis http://hdl.handle.net/1721.1/13550 24035893 eng 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 ix, 97 leaves 5476185 bytes 5475942 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology
spellingShingle Aeronautics and Astronautics
Mandell, Gordon Keith
Analysis of free-edge effects in composite laminates by an assumed-stress method.
title Analysis of free-edge effects in composite laminates by an assumed-stress method.
title_full Analysis of free-edge effects in composite laminates by an assumed-stress method.
title_fullStr Analysis of free-edge effects in composite laminates by an assumed-stress method.
title_full_unstemmed Analysis of free-edge effects in composite laminates by an assumed-stress method.
title_short Analysis of free-edge effects in composite laminates by an assumed-stress method.
title_sort analysis of free edge effects in composite laminates by an assumed stress method
topic Aeronautics and Astronautics
url http://hdl.handle.net/1721.1/13550
work_keys_str_mv AT mandellgordonkeith analysisoffreeedgeeffectsincompositelaminatesbyanassumedstressmethod