全文获取类型
收费全文 | 257篇 |
免费 | 59篇 |
国内免费 | 44篇 |
专业分类
航空 | 170篇 |
航天技术 | 63篇 |
综合类 | 35篇 |
航天 | 92篇 |
出版年
2024年 | 1篇 |
2023年 | 12篇 |
2022年 | 13篇 |
2021年 | 11篇 |
2020年 | 13篇 |
2019年 | 20篇 |
2018年 | 17篇 |
2017年 | 17篇 |
2016年 | 19篇 |
2015年 | 19篇 |
2014年 | 22篇 |
2013年 | 8篇 |
2012年 | 21篇 |
2011年 | 20篇 |
2010年 | 12篇 |
2009年 | 11篇 |
2008年 | 13篇 |
2007年 | 17篇 |
2006年 | 14篇 |
2005年 | 14篇 |
2004年 | 12篇 |
2003年 | 5篇 |
2002年 | 10篇 |
2001年 | 8篇 |
2000年 | 10篇 |
1999年 | 3篇 |
1998年 | 4篇 |
1997年 | 3篇 |
1995年 | 2篇 |
1994年 | 2篇 |
1992年 | 1篇 |
1991年 | 1篇 |
1990年 | 3篇 |
1989年 | 2篇 |
排序方式: 共有360条查询结果,搜索用时 62 毫秒
81.
《中国航空学报》2019,32(9):2211-2221
Carbon fiber reinforced plastic and titanium alloy (CFRP/Ti) stacks have been widely used as aerospace structures because of their excellent combination of physical properties. Interface damage caused by interface gaps, significantly different from that of metal/metal stacks, is a common problem in the through-hole drilling of CFRP/Ti stacks with low stiffness. In this study, a force–deformation coupling model was developed to further examine the formation mechanism and the control method of interface damage. Firstly, the coupling model was built considering the interaction between the thrust force and the deformation. To solve this model, a numerical method was proposed in which specific cutting coefficients were calibrated using only the thrust force of rigid stacks. Secondly, drilling experiments were performed with different feed rates and bending stiffness. Experimental results indicate that interface damage mainly includes interlayer chips and surface damage of CFRP layers. The surface damage, which is irreparable, is caused by the rotary extension of metal chips along the interlayer gap. Thirdly, variations of the interface gap were calculated with the coupling model that had been verified by measured thrust forces. The damage area was found to have a linear dependence relation with the interlayer gap. However, in conditions of large gap sizes, the interface damage areas increased with the interlayer gap at high feed rates, while decreasing slightly at low feed rates. This phenomenon was satisfactorily explained by the presented model. Finally, a method was proposed to determine the appropriate pressure exceeding which no interlayer damage will occur. Additional drilling experiments proved the method effective. This study leads to further understanding of the forming mechanism of interlayer damage and of selecting appropriate parameters in drilling low-stiffness composite/metal stacks. 相似文献
82.
83.
84.
用矩量法(MOM)导出求解X波段波导端头裂缝单元间互耦等效磁流的模型。在此基础上给出了等效磁流在激励和未激励单元内部产生的场、反射系数、驻波系数和两单元间耦合系数等的计算公式。分别在共E、H面条件下分析了两X波段波导端头裂缝互耦的影响,并对单元间不同相对距离和工作频率时的互耦影响规律进行了讨论。研究结果表明,该算法简单,计算值与测试结果吻合较好。 相似文献
85.
介绍一种新型的遥测系统——桥函数遥测系统构成的基本思想,给出实验室样机的详细框图。并从理论和实验的角度分析比较了系统基带传输时各方面的性能。从而初步证明了具有三值的桥函数,作为遥测系统的副载波函数的可行性。 相似文献
86.
87.
To obtain high-quality aviation forgings of titanium alloys, β forging is an essential processing step which must be considered throughout a production process. In this work, the effect of β forging on the crystal orientation and morphology of lamellar α was experimentally investigated in a two-phase titanium alloy. Strong dynamic recovery during β working resulted in the formation of low-angle grain boundary (LAGBβ) inside β grains. The lamellar α can penetrate through the LAGBβ, leading to similar intra α LAGBs on subgrain boundaries. Deformation banding occurs at high strain rates, and both diffusive and sharp boundaries of deformation bands can be observed. A continuous change of the β orientation in diffusive boundaries results in the formation of fine and disordered α lamellae without intra-lamellar boundary to hold the Burgers orientation relationship (OR). On sharp boundaries, it is prone to producing continuous grain boundary α (αGB) with a highly similar orientation along the boundaries. Meanwhile, there may exist several lower-angle boundaries within the grain boundary α for a smoother orientation change on the β grain boundary. 相似文献
88.
展成电解加工整体叶轮扭曲叶片中的间隙分析 总被引:1,自引:0,他引:1
叙述了展成电解加工整体叶轮扭曲叶片中间隙的计算方法,并讨论了工件和阴极各运动速度对间隙的影响。 相似文献
89.
90.