Finite element alternating analysis for stiffened fuselage with cracks

Bibliographic Details
Main Author:	Ogiso, Tadashi
Published:	Georgia Institute of Technology 2008
Subjects:	Fracture mechanics Finite element method
Online Access:	http://hdl.handle.net/1853/18992

id	ndltd-GATECH-oai-smartech.gatech.edu-1853-18992
record_format	oai_dc
spelling	ndltd-GATECH-oai-smartech.gatech.edu-1853-189922013-12-15T03:37:01ZFinite element alternating analysis for stiffened fuselage with cracksOgiso, TadashiFracture mechanicsFinite element methodGeorgia Institute of Technology2008-01-17T12:31:59Z2008-01-17T12:31:59Z1990-12Thesishttp://hdl.handle.net/1853/18992340412Access restricted to authorized Georgia Tech users only.
collection	NDLTD
sources	NDLTD
topic	Fracture mechanics Finite element method
spellingShingle	Fracture mechanics Finite element method Ogiso, Tadashi Finite element alternating analysis for stiffened fuselage with cracks
author	Ogiso, Tadashi
author_facet	Ogiso, Tadashi
author_sort	Ogiso, Tadashi
title	Finite element alternating analysis for stiffened fuselage with cracks
title_short	Finite element alternating analysis for stiffened fuselage with cracks
title_full	Finite element alternating analysis for stiffened fuselage with cracks
title_fullStr	Finite element alternating analysis for stiffened fuselage with cracks
title_full_unstemmed	Finite element alternating analysis for stiffened fuselage with cracks
title_sort	finite element alternating analysis for stiffened fuselage with cracks
publisher	Georgia Institute of Technology
publishDate	2008
url	http://hdl.handle.net/1853/18992
work_keys_str_mv	AT ogisotadashi finiteelementalternatinganalysisforstiffenedfuselagewithcracks
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