NASA Logo

NTRS

NTRS - NASA Technical Reports Server

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

Back to Results
Assessment of computational models for multilayered composite cylindersA study is made of the effects of variation in the lamination and geometric parameters of multilayered composite cylinders on the accuracy of the static and vibrational responses predicted by eight modeling approaches, based on two-dimensional shear-deformation shell theories. The standard of comparison is taken to be the exact three-dimensional elasticity solutions, and the quantities compared include both the gross response characteristics and detailed, through-the-thickness, distributions of displacements, stresses and strain energy densities. Based on the numerical studies conducted, a predictor-corrector approach, used in conjunction with the first-order shear-deformation theory (with five displacement parameters in the predictor phase), appears to be the most effective among the eight modeling approaches considered. For multilayered orthotropic cylinders the response quantities obtained by the predictor-corrector approach are shown to be in close agreement with the exact three-dimensional elasticity solutions for a wide range of lamination and geometric parameters.
Document ID
19900059244
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Noor, A. K.
(NASA Langley Research Center Hampton, VA, United States)
Burton, W. S.
(NASA Langley Research Center Hampton, VA, United States)
Peters, J. M.
(NASA Langley Research Center; George Washington University Hampton, VA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Structural Mechanics
Meeting Information
Meeting: ASME Winter Annual Meeting
Location: San Francisco, CA
Country: United States
Start Date: December 10, 1989
End Date: December 15, 1989
Sponsors: ASME
Accession Number
90A46299
Funding Number(s)
CONTRACT_GRANT: NAG1-788
CONTRACT_GRANT: AF-AFOSR-87-0115
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available