Titlebook: Composite Structures; I. H. Marshall Book 1991 Elsevier Science Publishers LTD 1991 cement.composite.composite material.deformation.fatigu

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Reliability Analysis for Transient Stress Wave in Elastic Laminated Composites, rate of change in the mean stresses, and indicate the peak at the position close to the wave fronts. The peak values account for the high rates significant for the mean stress values. This means that the stress waves propagate under considerably large probabilistic variations.

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Finite Element and Experimental Studies on an Orthotropic Disc,d and compared with finite element results. A reasonable degree of agreement is seen between the two. In the dynamic tests, the natural frequencies of the disc are found by experiment as well as by the finite element method. Here, too, a reasonable degree of agreement is seen.

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Repair of Delaminations and Impact Damage in Composite Aircraft Structures, of the repaired laminates to sustain (a) in-plane compression loads, (b) interlaminar shear loads, and (c) low velocity impact. The experimental results support the conclusion that resin injection can be a very effective means of repairing delaminations.

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Hygrothermal Effects on the Linear and Nonlinear Analysis of Composite Plates,e classical laminated plate theory may be inadequate for the analysis of several composite laminates, even in a small deflection range. The influence of the temperature variation, thickness and angle of the angle ply laminates on the errors of the analysis is evaluated.

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Effect of Water Temperature on Hygrothermal Aging of GFRP Panel, changes and bending properties are measured. The water temperature affects the weight changes but it never affects the changes in bending properties against weight gain. Moreover the difference in the degradation progress in the thickness direction is clear from the results of the ‘one side immersion test’.

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