| 1. | Peeling analysis of unperforated honeycomb structure
无孔蜂窝夹层结构脱粘剥离应力分析 |
| 2. | The above program in this paper has laid a theoretical foundation of the design of the stress release boot
本文所采用的方法可供今后人工脱粘层的设计参考。 |
| 3. | Elastoplastic behavior of particle reinforced metal matrix composites considering the interfacial debonding
有界面脱粘时颗粒增强金属基复合材料的弹塑性性能分析 |
| 4. | Decohesion and sliding are enhanced thanks to the anisotropy if the graphite sheets at the interphase / matrix interface
而3d - c sic中界面处热解碳层的各向异性结构会促进界面层的脱粘和滑动。 |
| 5. | Then the change of shear stress in the interface is deduced in theoretical way after the fibers are disengaged and pulled out from concrete
从理论方面计算了纤维受力后在脱粘和拔出过程中界面剪应力的变化。 |
| 6. | Hence , it is very significant to analyze the mechanism and extend law of interface debond of solid rocket motor
因此,研究固体火箭发动机界面脱粘的机理和扩展规律,是固体火箭发动机结构完整性分析的重要课题。 |
| 7. | To simulate the quiescence and flying status of the motor , the ablation is calculated with different cavity width
为模拟发动机静止与飞行两种不同状态，本文对不同宽度的槽缝人工脱粘层的烧蚀进行了计算，对其进行了比较。 |
| 8. | Interface debond between propellant and liner is a key form of failure of the structure integrity in the analysis of solid rocket motor
在固体火箭发动机结构完整性分析中,衬层/推进剂药柱粘接界面的脱粘是完整性被破坏的关键形式之一。 |
| 9. | This kind of positive feedback may extend the debonded area and result in out of control of pressure on the firebox , or even the explosion of the motor
这种正反馈可能使脱粘面进一步扩展,导致出现燃烧室压力失控甚至发动机爆炸的灾难性后果。 |
| 10. | After igniting the motor , the combustion gas coming into the debond cavity may expand the debond cavity , and make an additional combustion area and lead to larger load
发动机点火后燃气进入脱粘腔,使脱粘腔变形并获得额外的燃烧面积,从而导致更强的载荷。 |
