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Optimized cross-ply orientation in aircraft wing skin
Optimized cross-ply orientation in aircraft wing skin
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机译:优化机翼蒙皮中的交叉层定向
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摘要
A composite laminate has a primary axis of loading and comprises a plurality resin plies each reinforced with unidirectional fibers. The laminate includes cross-plies with fiber orientations optimized to resist bending and torsional loads along the primary axis of loading.
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