首页> 美国卫生研究院文献>Heliyon >Effect of through thickness separation of fiber orientation on low velocity impact response of thin composite laminates
【2h】

Effect of through thickness separation of fiber orientation on low velocity impact response of thin composite laminates

机译:纤维取向通过厚度分离对复合材料薄板低速冲击响应的影响

代理获取
本网站仅为用户提供外文OA文献查询和代理获取服务,本网站没有原文。下单后我们将采用程序或人工为您竭诚获取高质量的原文,但由于OA文献来源多样且变更频繁,仍可能出现获取不到、文献不完整或与标题不符等情况,如果获取不到我们将提供退款服务。请知悉。

摘要

The effect of separation of fiber orientation through the thickness of thin composites on their low velocity impact response is studied. The composites are prepared using unidirectional glass fiber reinforced epoxy through hand layup followed by vacuum bagging. The two dissimilar layups of composites considered have separation of composite layers with fibers having the same and different orientations through the thickness. The composites are subjected to low velocity impact using a drop-weight testing machine. The composites are evaluated using different performance parameters such as damage degree, first damage and maximum forces, first cracking energy, bending stiffness, elastic strain energy, elastic, residual and maximum displacements, permanent deformation, square-root delaminated area, delamination length and width, and contact duration. Among the two composites, it is observed that [90/-45/45/0] composite in which two layers with fibers having 90° and 0° orientations separating by two layers with fibers having -45° and 45° orientations, levels of deformation are lower and recorded force and square-root delaminated area are higher and lower, respectively for the same level of impact energy. Whereas, in case of [0/90/90/0] composite in which two layers with fibers having 0° orientations separating by two layers with fibers having 90° orientations, recorded force is lower and deformation and square-root delaminated area are higher. The [0/90/90/0] composite is having a comparatively more lateral spread of delamination and inter-layer opening than that of [90/-45/45/0] composite considering extensional and bending stiffnesses along longitudinal (A , D ) and transverse (A , D ) directions. This facilitates that lateral spread of damage within composite can be decreased by separating two layers of composite with 90° and 0° fiber orientations by two layers with -45° and 45° fiber orientations, i.e., [90/-45/45/0] composite.
机译:研究了通过薄复合材料厚度分离纤维取向对其低速冲击响应的影响。复合材料是使用单向玻璃纤维增​​强环氧树脂通过手工铺层,然后进行真空装袋来制备的。所考虑的两个不同的复合物叠层将复合物层与纤维在厚度方向上具有相同和不同的方向分开。使用落锤试验机对复合材料进行低速冲击。使用不同的性能参数对复合材料进行评估,例如破坏程度,首次破坏和最大力,首次破裂能,弯曲刚度,弹性应变能,弹性,残余和最大位移,永久变形,平方根分层面积,分层长度和宽度,以及联系时间。在两种复合物中,观察到[90 / -45 / 45/0]复合物,其中具有90°和0°取向的纤维的两层被具有-45°和45°取向的纤维的两层分开,在相同水平的冲击能量下,变形较低,记录的力和平方根分层面积分别较高和较低。而在[0/90/90/0]复合材料中,具有0°取向的纤维的两层被具有90°取向的纤维的两层分开,记录的力较低,并且变形和平方根分层面积较高。考虑到沿纵向的拉伸和弯曲刚度,[0/90/90/0]复合材料的分层和层间开口的横向扩展比[90 / -45 / 45/0]复合材料的横向扩展更大。 )和横向(A,D)方向。这有助于通过将纤维方向为90°和0°的两层复合材料与纤维方向为-45°和45°的两层分开,即[90 / -45 / 45/0 ]复合材料。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
代理获取

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号