NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Probabilistic assessment of composite structuresA methodology and attendant computer code were developed and are used to computationally simulate the uncertain behavior of composite structures. The uncertain behavior includes buckling loads, stress concentration factors, displacements, stress/strain, etc., which are the consequences of the inherent uncertainties (scatter) in the primitive (independent random) variables (constituent, ply, laminate, and structural) that describe the composite structures. The computer code is IPACS (Integrated Probabilistic Assessment of Composite Structures). IPACS can simulate both composite mechanics and composite structural behavior. Application to probabilistic composite mechanics is illustrated by its use to evaluate the uncertainties in the major Poisson's ratio and in laminate stiffness and strength. IPACS' application to probabilistic structural analysis is illustrated by its used to evaluate the uncertainties in the buckling of a composite plate, the stress concentration factor in a composite panel, and the vertical displacement and ply stress in a composite aircraft wing segment. IPACS' application to probabilistic design is illustrated by its use to assess the thin composite shell (pipe).
Document ID
19930017903
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Chamis, C. C.
(NASA Lewis Research Center Cleveland, OH, United States)
Shiao, Michael C.
(Sverdrup Technology, Inc. Brook Park, OH., United States)
Date Acquired
September 6, 2013
Publication Date
February 1, 1993
Subject Category
Composite Materials
Report/Patent Number
NAS 1.15:106024
E-7587
NASA-TM-106024
Report Number: NAS 1.15:106024
Report Number: E-7587
Report Number: NASA-TM-106024
Accession Number
93N27092
Funding Number(s)
PROJECT: RTOP 510-02-12
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available