| 1. | Interlaminar stress and damage mechanism of thermoplastic composite laminates
热塑性复合材料层合板的层间应力与损伤机理 |
| 2. | Interlaminar stress analysis of composite laminates subjected to in - plane loading
受面内载荷的层压复合材料的层间应力分析 |
| 3. | Interlaminar stress analysis of the thick thermoplastic as4 peek angle - ply composite laminates
角铺设层合板的层间应力分析 |
| 4. | Effect of gradient of fiber laminates on flexural rigidity and interlaminar stress
纤维层合板梯度化后对弯曲刚度与层间应力的影响 |
| 5. | This paper also offers the methematics analyzing method of how to calculate interlaminar stresses according to the finite element analyzing method , it helps to do deeper research on composite materials shells
并结合有限元分析法提出了计算层间应力的数值分析方法，有助于对复合材料层合板壳进行深入的研究。 |
| 6. | Firstly , the interlaminar stresses of composite materials shell is analyzed , and the destructive influence of the actual structure of composite materials of distribution of composite materials shell ' s interlaminar stresses is raised in this paper
本文首先对复合材料壳体的层间应力进行分析，提出了复合材料壳体层间应力分布对复合材料实际结构破坏的影响。 |
| 7. | Secondly , the finite element analysis of composite materials interlaminar stresses is researched in this paper . the interlaminar stresses slightly influenced by the composite materials ' lamella curvature , but not influenced by the distributing form of interlaminar stresses follow thickness are found
本文在研究复合材料层间应力的有限元分析时，发现复合材料层合壳曲率对层间应力大小有一定影响，但对层间应力沿厚度的分布形式影响不大。 |
| 8. | Based on the temperature field obtained by the thermal analysis , a parametric analysis is conducted to investigate the interlaminar stress at the interface between the composite and the thermal barrier in the cross - section of the inlet duct , using the commercial finite element software ansys
在热分析的基础上,采用ansys有限元软件计算了复合材料进气道截面在假设工况下的应力场,为碳纤维缠绕复合材料进气道热防护方案的设计提供了实用的参考依据。 |
| 9. | Fiber enlaced composite materials is widely used in engineering project . the mechanics property of the shell is rather complicated when analyzing the affect of composite materials shell ' s interlaminar stresses . the result shows that the interlaminar stresses of composite materials shell will be changed much according to the change of the fiber direction , not only the distribution style , but also the interface which the maxinal interlaminar shearing stresses belongs to
纤维缠绕复合材料壳体在工程实际中得到广泛应用，其壳体力学性能相当复杂，本文在分析复合材料壳体层间应力的影响时，提出了复合材料壳体层间应力随纤维方向的改变有较大的不同，不仅分布形式不同，其最大层间剪应力所在的界面也各不相同。 |
| 10. | By means of the calculation results of interlaminar stress distributions , the influence of delamination growth on the resultant fatigue lives is qualitatively discussed , realizing that a more comprehensive analytical model is essential to include the effect of stacking sequence and the arosing interlamina stresses on fatigue behaviors of laminates . the recommended scheme was also used to calculate the fatigue lives of specimens with central holes subjected tensile - compressive cyclic loadings and has got comparable estimations with experimental results
发现和修正了有关文献中的一些错误，重新建立了断裂筋条弯曲修正的公式和位移协调方程，编制了相应的计算程序，根据计算结果探讨了断裂筋条和筋条弯曲对蒙皮裂纹的影响，指出了有的文献上给出的计算曲线存在的谬误。 |
