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Buckling of conical shell with local imperfectionsSmall geometric imperfections in thin-walled shell structures can cause large reductions in buckling strength. Most imperfections found in structures are neither axisymmetric nor have the shape of buckling modes but rather occur locally. This report presents the results of a study of the effect of local imperfections on the critical buckling load of a specific axially compressed thin-walled conical shell. The buckling calculations were performed by using a two-dimensional shell analysis program referred to as the STAGS (Structural Analysis of General Shells) computer code, which has no axisymmetry restrictions. Results show that the buckling load found from a bifurcation buckling analysis is highly dependent on the circumferential arc length of the imperfection type studied. As the circumferential arc length of the imperfection is increased, a reduction of up to 50 percent of the critical load of the perfect shell can occur. The buckling load of the cone with an axisymmetric imperfections is nearly equal to the buckling load of imperfections which extended 60 deg or more around the circumference, but would give a highly conservative estimate of the buckling load of a shell with an imperfection of a more local nature.
Document ID
19740021200
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Cooper, P. A.
(NASA Langley Research Center Hampton, VA, United States)
Dexter, C. B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1974
Subject Category
Structural Mechanics
Report/Patent Number
L-9331
NASA-TM-X-2991
Report Number: L-9331
Report Number: NASA-TM-X-2991
Accession Number
74N29313
Funding Number(s)
PROJECT: RTOP 743-32-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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