Investigation of Through-Thickness Stresses in Composite Laminates Using Layerwise Theory

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</svg> on through-thickness of the [0°/60°/−60°]<sub><i>s</i></sub> laminate as a function of layer subdivision number <svg height="13.3" id="M150" style="vertical-align:-3.50804pt" version="1.1" viewbox="0 0 10.2 13.3" width="10.2" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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International Journal of Engineering Mathematics

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Figure 7

Figure 7: Investigation of Through-Thickness Stresses in Composite Laminates Using Layerwise Theory 