| 1. | Carbon fibre laminates - determination of the fibre , resin and void contents
碳纤维层压板材.纤维树脂含量和空隙率的测定 |
| 2. | The bending strength of fiber / resin / aluminum alloy laminated composites is 465mpa and it has good property of bend formability
纤维树脂铝合金叠层复合材料具有良好的弯曲性能，弯曲强度达465mpa ，加工成型性好。 |
| 3. | The interface bonding of laminated composites is analyzed by using a method of shear strength and t - peel off strength
通过剪切强度和t ?剥离强度直观的分析了纤维树脂铝合金叠层复合材料中铝-树脂界面的结合情况。 |
| 4. | The fiber / resin / aluminum alloy laminated composites have been fabricated by using a method of hot pressing and solidifying . the interface bonding strength of aluminum alloy / resin interface , mechanical property and anti - vibration damping property are investigated
采用热压固化法制备了纤维树脂铝合金叠层复合材料，并研究其界面结合、力学性能及抗振阻尼性能。 |
| 5. | Fiber / resin / aluminum alloy laminated composites is a kind of interlaminar superhybrid composite material developed by laminating fiber , resin and aluminum alloy . it has not only the property of polymer composites but also that of aluminum alloy
纤维树脂铝合金叠层复合材料是由纤维、树脂、铝合金叠层复合而成的层间超混杂复合材料，它既保持了树脂复合材料的性能又兼具铝合金的性能。 |
| 6. | The damping coefficient of the laminated composites is more than twice that of ly12 aluminum alloy . furthermore , the damping coefficient of laminated composite is enhanced with the increasing of thickness of fiber / resin layer . the vibration damping mechanism is analyzed
研究了不同纤维树脂层厚度时叠层复合材料的阻尼性能，发现随中间层厚度的增加，叠层复合材料的振动衰减系数增加，并分析其振动衰减机制。 |
| 7. | In this paper , single fiber composite fragment ( sfc ) method , which is one of the most widespread and effective experimental methods for determining the mechanical properties of interface , was adopted to study the load transfer mechanism and to evaluate the adhesion performance of composite with surface - treated fibers . this is helpful for optimization design of interface
本文采用了目前最为流行、最为有效的直接测定界面力学性能的实验方法之一? ?单纤维复合材料断裂实验研究了纤维树脂界面载荷传递机理，分析了几种纤维表面处理复合材料界面的粘结情况，对界面的优化设计具有一定的指导作用。 |
