Sentence examples for laminate skin from inspiring English sources

and a conventional two-dimensional (2D) tape laminate T-stiffener, bonded onto a tape laminate skin.

The ply orientations and materials of the woven composite laminate skin are varied.

This paper summarizes the results of experimental and numerical studies on the flexural behavior of stitched foam core carbon/epoxy laminate skin sandwich structure.

The sandwich panels were assembled with bonded laminate skins.

The body of a satellite consists of a monocoque structure formed by joining several composite sandwich panels composed of an aluminum honeycomb core with carbon fiber reinforced laminate skins on both sides.

This work deals with the analysis of the mechanical behaviour of a class of sandwich structures widely employed in marine constructions, constituted by fiber-glass laminate skins over PVC foam or polyester mat cores.

A systematic experimental study to determine the effect of curvatures and debond on the flexural stiffness and strength of composite sandwich beam structures made from fiber-glass/epoxy laminate skins and polyurethane foam core has been carried out.

The numerical accuracy of the model was assessed using data obtained from fire structural tests performed on a combustible sandwich composite consisting of thin woven glass vinyl ester laminate skins and a thick core of balsa wood.

These tanks encompassed several challenging design features: (1) one-piece co-cured/co-bonded spherical geometry with integral fluted core skirt, (2) out-of-autoclave (OoA) curing carbon/epoxy (C/E) materials, (3) permeation resistant thin ply hybrid laminate skins, and (4) off-axis slit-tape tow (STT) construction.

The specimens composed of a laminate (the skin) to which an over-thickness (the flange) had been added were subjected to four-point bending, which led to interface failure between the flange and the skin.

The aim of this research is to analyse the failure of a Fiber Metal Laminate (FML) skin adhesively bonded to a Carbon Fiber Reinforced Polymer (CFRP) stiffener, under quasi-static loading at different environmental temperatures (−55 °C, Room Temperature RT and +100 °C) and under fatigue loading at RT.