全文获取类型
收费全文 | 2735篇 |
免费 | 347篇 |
国内免费 | 497篇 |
专业分类
航空 | 1560篇 |
航天技术 | 739篇 |
综合类 | 586篇 |
航天 | 694篇 |
出版年
2024年 | 3篇 |
2023年 | 9篇 |
2022年 | 23篇 |
2021年 | 41篇 |
2020年 | 48篇 |
2019年 | 24篇 |
2018年 | 28篇 |
2017年 | 22篇 |
2016年 | 49篇 |
2015年 | 60篇 |
2014年 | 120篇 |
2013年 | 127篇 |
2012年 | 129篇 |
2011年 | 169篇 |
2010年 | 177篇 |
2009年 | 144篇 |
2008年 | 181篇 |
2007年 | 178篇 |
2006年 | 125篇 |
2005年 | 124篇 |
2004年 | 78篇 |
2003年 | 101篇 |
2002年 | 88篇 |
2001年 | 118篇 |
2000年 | 114篇 |
1999年 | 156篇 |
1998年 | 162篇 |
1997年 | 139篇 |
1996年 | 118篇 |
1995年 | 106篇 |
1994年 | 113篇 |
1993年 | 102篇 |
1992年 | 87篇 |
1991年 | 75篇 |
1990年 | 61篇 |
1989年 | 54篇 |
1988年 | 28篇 |
1987年 | 42篇 |
1986年 | 9篇 |
1985年 | 11篇 |
1984年 | 8篇 |
1983年 | 6篇 |
1982年 | 15篇 |
1981年 | 4篇 |
1980年 | 1篇 |
1965年 | 2篇 |
排序方式: 共有3579条查询结果,搜索用时 375 毫秒
671.
基于静强度分布的复合材料疲劳寿命分布的预测模型(英文) 总被引:4,自引:2,他引:2
The reasons of the static strength dispersion and the fatigue life dispersion of composite laminates are analyzed in this article. It is concluded that the inner original defects, which derived from the manufacturing process of composite laminates, are the common and major reason of causing the random distributions of the static strength and the fatigue life. And there is a correlative relation between the two distributions. With the study of statistical relationship between the fatigue loading and the fatigue life in the uniform confidence level and the same survival rate S-N curves of material, the relationship between the static strength distribution and the fatigue life distribution through a material S-N curve model has been obtained. And then the model which is used to describe the distributions of fatigue life of composites, based on their distributions of static strength, is set up. This model reasonably reflects the effects of the inner original defects on the static strength dispersion and on the fatigue life dispersion of composite laminates. The experimental data of three kinds of composite laminates are employed to verify this model, and the results show that this model can predict the random distributions of fatigue life for composites under any fatigue loads fairly well. 相似文献
672.
673.
674.
675.
小型热真空试验设备网络化集群测控技术 总被引:3,自引:1,他引:2
随着航天器部组件试验任务的日益增多,在人员少的情况下,高效率地完成型号任务的需求十分迫切。文章介绍了小型热真空试验设备网络化集群测控的方法与技术,以某小型热真空试验设备群为例,针对其接口复杂、数据量大、地理位置分散且要求集中管理的特点,详细阐述了采用混合B/S模式与C/S模式的网络化测控技术来实现小型热真空试验设备群集群测控的功能。该技术已在小型热真空试验设备的集群控制中得到了成功的应用。 相似文献
676.
微课不是指用于微学习的微内容,而是指使用专业软件构建便于在线和移动学习的实际教学内容。笔者结合教学实践,利用iSpring Suite软件制作微课,开展对材料成型专业英语的教学研究,并进一步探索基于微课的翻转课堂教学模式。 相似文献
678.
679.
Wen-jie Wang Ze-ping Wu Dong-hui Wang Wei-hua Zhang Kun Zhao Patrick N. Okolo Gareth J. Bennett 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(11):3706-3720
Hypersonic vehicles are receiving increased attention within the aerospace community due to their high cruise speed and long-range capabilities. In this paper, a modified Sequential Approximate Optimization method is proposed for an optimized aerodynamic design of a hypersonic vehicle. As part of this approach, a constrained experimental design method is developed to handle the constraints more efficiently. A radial basis function is used to surrogate time-consuming CFD analysis. An efficient and more robust numerical mesh morphing scheme for the hypersonic vehicle is developed for the generation of high-quality meshes. Within this paper, a novel adaptive infilling strategy is proposed which uses an inaccurate search technique coupled with an elite archive. This allows the location of a more promising sample region and hence improves the surrogate accuracy, thereby further enhancing the optimization efficiency. A hypersonic vehicle aerodynamic design problem is solved using the proposed approach and satisfactory results are obtained at much lower computational costs. The lift-to-drag ratio is increased by 23.8% when compared with the base configuration while also satisfying the volume and lift constraints. The pressure and Mach contours have been compared with those of the base configuration and the results demonstrate the strength of the optimized configuration. The modified sequential approximate optimization for designing an improved hypersonic vehicle is worth referencing in future work. 相似文献
680.
陆空通话是航指挥的基本功,它为航管人员与飞行员信息勾通架起一座桥梁。本文介绍利用计算机多媒体技术开发的人机标准陆空通话自学习系统,它可以根据学员自身的学习效果,控制学习进度。该系统可以有效地促进、提高学员的听说能力。 相似文献