| 1. | Standard practice for fracture toughness testing of aluminum alloys
铝合金断裂韧性试验的标准实施规程 |
| 2. | Standard practice for plane - strain fracture toughness testing of aluminum alloys
铝合金的平面应变断裂韧性试验的标准实施规程 |
| 3. | Standard guide for plane strain fracture toughness testing of non - stress relieved aluminum products
非应力消除铝制品的平面应力断裂强度试验的标准导则 |
| 4. | Prefabricating original cracks in refractory specimens for fracture toughness test using high temperature static fatigue method
高温静疲劳法预制耐火材料断裂韧性试件原生裂纹 |
| 5. | Using the modal taking into effects of the notch width . , this paper also compute the stress intensity factor of ccnbd suggest by isrm for rock fracture toughness test . and some conclusions have been made in this research
本文还对国际岩石力学学会( isrm ) 95年方法推荐的ccnbd断裂韧度试样采用考虑切槽宽度的模型进行了计算，得到一些有意义的结论。 |
| 6. | Combining the fracture toughness test results of rcc specimens with the existed size effect formula for fracture toughness of common concrete , the suitable size effect formula fur fracture toughness of rcc was gotten on the comparative of results of the computation models
将碾压混凝土断裂韧度试验结果与已有的普通混凝土断裂韧度尺寸效应公式结合，通过对几种模型的计算结果的分析比较，得到了碾压混凝土所适用的断裂韧度尺寸效应公式。 |
| 7. | Therefore , interlayer toughened composites are the excellent candidate materials for primary structure of aircrafts . in this paper , composites modified with particle - interlayer were fabricated . based on the aims of improving compression strength after impact ( cai ) and evaluate damage resistance and damage tolerance , mode ii fracture toughness test and quasi - static indentation test ( qsi ) were conducted
本文采用层间颗粒增韧技术制备试验件，基于提高冲击后压缩强度( cai )和考察损伤阻抗、损伤容限的目的，试验测试了型层间断裂韧性g _ ( c ) 、准静压痕( qsi )试验的分层起始能量和接触力?凹坑深度关系。 |
