Abstract
A global shared-layer blending (GSLB) method is proposed for obtaining manufacturable stacking sequence of composite structures with blending and design rules. The method combines the traditional SLB technique with an evaluation algorithm of spatial variation of panels, where the manufacturability of laminates is enhanced by identifying and minimizing the ply-drops, and controlling the laminate transition drop boundaries. In addition, a blended design scheme is also proposed, which is achieved by using the stacking sequence table technique. A composite wing structure is selected to validate the efficiency and accuracy of the proposed method. Results show that the GSLB method can be used for generating more manufacturable designs of large-scale composite structure with multiple engineering constraints.
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Jing, Z., Fan, X., & Sun, Q. (2015). Global shared-layer blending method for stacking sequence optimization design and blending of composite structures. Composites Part B: Engineering, 69, 181–190. https://doi.org/10.1016/j.compositesb.2014.09.039
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