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Flat nose low velocity drop-weight impact response of carbon fibre composites using non-destructive damage detection techniques

机译:无损损伤检测技术对碳纤维复合材料扁鼻低速降重的冲击响应

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This work is mainly concerned with the nondestructive post-impact damage evaluation of carbon fibre reinforced laminated composite panels subject to low velocity drop-weight impact by flat and round nose impactors. Quasi-isotropic laminates consisting of eight-, sixteen-, and twenty-four plies were impacted by flat and round nose impactors at different velocity levels. Load-time history data were recorded and plotted to correlate loaddrop as damage level to the impactor nose profiles. Test produced data, non-destructive damage detection techniques: visual, ultrasonic, and eddy- current, and computer simulations were utilised to identify and quantify status of the impact induced damage. To evaluate damage in relatively thick laminates (consisting of 24-Ply), the damage ratios and deflection quantities were correlated to the corresponding impactor nose profiles. Damage induced by the flat nose impactor to thick laminates was compared against the data produced by the round nose impactor. Results show that relatively thin laminates were largely affected by the impactor nose. Reasonable difference was observed in damage caused by flat and round impactor nose profiles to thick laminates impacted at relatively higher velocity impacts. Resultswere compared and validated against simulation produced data.
机译:这项工作主要涉及碳纤维增强层压复合板的无损冲击后评估,该复合材料受到扁平和圆鼻冲击器低速降重冲击。由八层,十六层和二十四层组成的准各向同性层压板受到扁平和圆形鼻冲击器在不同速度水平下的冲击。记录载荷时间历史数据并作图,以使载荷下降与冲击器鼻廓的损伤程度相关。测试产生的数据,非破坏性损坏检测技术:视觉,超声和涡流,以及计算机模拟被用来识别和量化撞击引起的损坏的状态。为了评估相对较厚的层压板(由24层组成)中的损伤,将损伤率和挠曲量与相应的冲击器鼻形相关联。将扁鼻子冲击器对厚层压板造成的损坏与圆鼻子冲击器产生的数据进行了比较。结果表明,相对较薄的层压板受撞击器鼻部的影响很大。在以相对较高的速度撞击时,平坦和圆形的冲击头鼻廓对厚的层压板造成的损害观察到合理的差异。将结果与模拟产生的数据进行比较和验证。

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