NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
An analytical study of the effects of transverse shear deformation and anisotropy on buckling loads of laminated cylindersBuckling loads of thick-walled orthotropic and anisotropic simply supported circular cylinders are predicted using a higher-order transverse-shear deformation theory. A comparison of buckling loads predicted by the conventional first-order transverse-shear deformation theory and the higher-order theory show that the additional allowance for transverse shear deformation has a negligible effect on the predicted buckling loads of medium-thick metallic isotropic cylinders. However, the higher-order theory predicts buckling loads which are significantly lower than those predicted by the first-order transverse-shear deformation theory for certain short, thick-walled cylinders which have low through-the-thickness shear moduli. A parametric study of the effects of ply orientation on the buckling load of axially compressed cylinders indicates that laminates containing 45 degree plies are most sensitive to transverse-shear deformation effects. Interaction curves for buckling loads of cylinders subjected to axial compressive and external pressure loadings indicate that buckling loads due to external pressure loadings are as sensitive to transverse-shear deformation effects as buckling loads due to axial compressive loadings. The effects of anisotropy are important over a much wider range of cylinder geometries than the effects of transverse shear deformation.
Document ID
19880004005
Document Type
Thesis/Dissertation
Authors
Jegley, Dawn C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1987
Subject Category
COMPOSITE MATERIALS
Report/Patent Number
NASA-TM-100508
NAS 1.15:100508
Funding Number(s)
PROJECT: RTOP 505-63-01-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Document Inquiry