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A probabilistic method for the buckling assessment of stiffened composite shellsA method is described to computationally simulate probabilistic buckling behavior of multilayered composite shells. The simulation accounts for all naturally-occurring uncertainties including those in constituent (fiber/matrix) material properties, fabrication variables, and structure geometry. The method is demonstrated for probabilistically assessing the buckling survivability of a specific case of a stiffened composite cylindrical shell with and without cutouts. The sensitivities of various uncertain variables on the buckling survivability are evaluated at specified reliability. The results show that the buckling survivability for a shell without cutouts depends primarily on shell skin related uncertainties. However, stringer related uncertainties become important for a shell with cutouts.
Document ID
19940008906
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Shiao, Michael C.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Abumeri, Galib H.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Singhal, Surendra N.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Chamis, Christos C.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1993
Subject Category
Structural Mechanics
Report/Patent Number
NASA-TM-106286
NAS 1.15:106286
E-8024
Report Number: NASA-TM-106286
Report Number: NAS 1.15:106286
Report Number: E-8024
Meeting Information
Meeting: International Conference on Composite Materials
Location: Madrid
Country: Spain
Start Date: July 12, 1993
End Date: July 16, 1993
Accession Number
94N13379
Funding Number(s)
PROJECT: RTOP 510-02-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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