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Global/local stress analysis of composite structuresA method for performing a global/local stress analysis is described and its capabilities are demonstrated. The method employs spline interpolation functions which satisfy the linear plate bending equation to determine displacements and rotations from a global model which are used as boundary conditions for the local model. Then, the local model is analyzed independent of the global model of the structure. This approach can be used to determine local, detailed stress states for specific structural regions using independent, refined local models which exploit information from less-refined global models. The method presented is not restricted to having a priori knowledge of the location of the regions requiring local detailed stress analysis. This approach also reduces the computational effort necessary to obtain the detailed stress state. Criteria for applying the method are developed. The effectiveness of the method is demonstrated using a classical stress concentration problem and a graphite-epoxy blade-stiffened panel with a discontinuous stiffener.
Document ID
19900001140
Acquisition Source
Legacy CDMS
Document Type
Thesis/Dissertation
Authors
Ransom, Jonathan B.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1989
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.15:101640
NASA-TM-101640
Report Number: NAS 1.15:101640
Report Number: NASA-TM-101640
Accession Number
90N10456
Funding Number(s)
PROJECT: RTOP 505-63-01-10
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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