Thin shell and new invariant elements by hybrid stress method
Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983.
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Format: | Thesis |
Language: | eng |
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Massachusetts Institute of Technology
2005
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Online Access: | http://hdl.handle.net/1721.1/15693 |
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author | Sumihara, Kiyohide |
author2 | Theodore H.H. Pian. |
author_facet | Theodore H.H. Pian. Sumihara, Kiyohide |
author_sort | Sumihara, Kiyohide |
collection | MIT |
description | Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983. |
first_indexed | 2024-09-23T13:35:02Z |
format | Thesis |
id | mit-1721.1/15693 |
institution | Massachusetts Institute of Technology |
language | eng |
last_indexed | 2024-09-23T13:35:02Z |
publishDate | 2005 |
publisher | Massachusetts Institute of Technology |
record_format | dspace |
spelling | mit-1721.1/156932019-04-10T13:47:35Z Thin shell and new invariant elements by hybrid stress method Sumihara, Kiyohide Theodore H.H. Pian. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics. Aeronautics and Astronautics. Thesis (Ph.D.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1983. MICROFICHE COPY AVAILABLE IN ARCHIVES AND AERO Vita. Includes bibliographical references. by Kiyohide Sumihara. Ph.D. 2005-08-04T22:11:20Z 2005-08-04T22:11:20Z 1983 1983 Thesis http://hdl.handle.net/1721.1/15693 10938676 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 [12], 203 leaves 8589773 bytes 8589527 bytes application/pdf application/pdf application/pdf Massachusetts Institute of Technology |
spellingShingle | Aeronautics and Astronautics. Sumihara, Kiyohide Thin shell and new invariant elements by hybrid stress method |
title | Thin shell and new invariant elements by hybrid stress method |
title_full | Thin shell and new invariant elements by hybrid stress method |
title_fullStr | Thin shell and new invariant elements by hybrid stress method |
title_full_unstemmed | Thin shell and new invariant elements by hybrid stress method |
title_short | Thin shell and new invariant elements by hybrid stress method |
title_sort | thin shell and new invariant elements by hybrid stress method |
topic | Aeronautics and Astronautics. |
url | http://hdl.handle.net/1721.1/15693 |
work_keys_str_mv | AT sumiharakiyohide thinshellandnewinvariantelementsbyhybridstressmethod |