全文获取类型
收费全文 | 354篇 |
免费 | 64篇 |
国内免费 | 89篇 |
专业分类
航空 | 318篇 |
航天技术 | 54篇 |
综合类 | 51篇 |
航天 | 84篇 |
出版年
2024年 | 3篇 |
2023年 | 13篇 |
2022年 | 7篇 |
2021年 | 20篇 |
2020年 | 15篇 |
2019年 | 13篇 |
2018年 | 15篇 |
2017年 | 18篇 |
2016年 | 41篇 |
2015年 | 10篇 |
2014年 | 14篇 |
2013年 | 11篇 |
2012年 | 28篇 |
2011年 | 29篇 |
2010年 | 19篇 |
2009年 | 26篇 |
2008年 | 24篇 |
2007年 | 26篇 |
2006年 | 22篇 |
2005年 | 14篇 |
2004年 | 22篇 |
2003年 | 13篇 |
2002年 | 17篇 |
2001年 | 10篇 |
2000年 | 10篇 |
1999年 | 13篇 |
1998年 | 12篇 |
1997年 | 7篇 |
1996年 | 9篇 |
1995年 | 5篇 |
1994年 | 4篇 |
1993年 | 4篇 |
1992年 | 7篇 |
1990年 | 3篇 |
1989年 | 2篇 |
1987年 | 1篇 |
排序方式: 共有507条查询结果,搜索用时 46 毫秒
81.
《中国航空学报》2020,33(10):2794-2806
The unsatisfied surface quality seriously impedes the wide application of incremental sheet forming (ISF) in industrial field. As a novel approach, the interpolator method is a promising strategy to enhance the surface quality in ISF. However, the mechanism for the improvement of surface quality and the influence of interpolator properties on surface roughness are not well understood. In this paper, the influences of process variables (i.e. tool diameter, step size and thickness of interpolators) on the forming process (e.g. surface roughness, forming force and geometric error) are investigated through a systematic experimental approach of central composite design (CCD) in two-point incremental sheet forming (TPIF). It is obtained that the increase in thickness of interpolators decreases the surface roughness in direction vertical to the tool path while increases the surface roughness in direction horizontal to the tool path. Nevertheless, the combined influence between thickness of interpolators and process parameters (tool diameter and step size) is limited. Meanwhile, the placement of interpolator has little influence on the effective forming force of blank. In addition, the geometric error enlarges with the increase of step size and thickness of interpolator while decreases firstly and then increase with an increase in tool diameter. Finally, the influencing mechanism of the interpolator method on surface quality can be attributed to the decrease of the contact pressure due to the increase of contact area with the unchanged contact force. Meanwhile, the interpolator method eliminates the sliding friction on the surface of blank due to the stable relative position between the blank and the interpolator. 相似文献
82.
83.
84.
85.
86.
AZ31镁合金板热成形中的屈服和损伤:本构实现与数值分析 总被引:1,自引:1,他引:0
为了准确预测各向异性镁合金板的成形质量,将改进的GTN损伤模型与各向异性拉压不对称的CPB06屈服本构耦合,并考虑了屈服面形状随塑性应变累积的变化,得到了考虑本构参数随塑性应变演化的各向异性屈服CPB06-GTN损伤模型。基于该模型,在ABAQUS/Explict中编译得到了相应的VUMAT子程序,采用单个单元进行了单轴拉伸和压缩模拟,并通过与实验一致性对比验证了子程序的正确性。使用子程序不仅能够模拟镁合金的各向异性屈服及其不规则的硬化,同时也能够模拟镁合金的损伤破坏。此外,采用编写的子程序进行了热拉深成形的数值模拟,模拟预测与实验结果对比表明,采用各向异性损伤模型的计算结果能够准确预测镁合金的变形及其损伤破坏,模拟结果与实验数据吻合;采用合适的压边力和成形的温度条件及非等温成形方法能够提高镁合金的成形性。 相似文献
87.
《中国航空学报》2021,34(4):253-264
In the 3D free bending forming system, the bending die can be designed either in a sliding type or rolling friction type. Bending die-based sliding friction type is often called normal bending dies; however, the bending dies-based rolling friction type includes bending die-based roller type and ball type in structure. In the current study, the impact of three bending dies on the forming force, and the bent tube quality was investigated. The obtained results showed that the tangential stresses and strains of the tubes formed by the bending die-based roller type were the smallest among the three bending dies. Besides, the spherical bearing force PU was reduced drastically after using the roller type and ball type compared to the sliding friction type. Moreover, the uniformity of the wall thickness distribution of the tubes formed by the roller type and ball type was better than those obtained from the sliding friction type. In addition, the cross-section distortion rate was reduced by 2.8% using the roller type, and 1.8% using ball-type compared to the sliding friction type. 相似文献
88.
89.
90.
设计并实现了一种基于双目立体视觉和数字图像相关方法的板料成形极限应变测量系统—BOSAS(双目视觉应变测量分析系统),对其中的关键技术作了深入讨论。该系统可以克服传统坐标网格方法很难进行变形过程的动态监控、自动化程度不高等局限,并可计算试件各变形阶段全场应变分布,以及重建不同变形时刻下试件的几何外形。将分段位移传递法和有限应变理论相结合,可计算大变形下的极限应变。对深冲铝板6016以及航空铝板2A12-T4、2A12-O、7B04-O等材料的应变测量结果显示本文方法适用于板料成形三维变形及极限应变的测量,并将测得数据与由坐标网格方法测得的数据进行比较,结果表明本文方法测量准确、可靠。 相似文献