全文获取类型
收费全文 | 920篇 |
免费 | 189篇 |
国内免费 | 313篇 |
专业分类
航空 | 874篇 |
航天技术 | 138篇 |
综合类 | 145篇 |
航天 | 265篇 |
出版年
2024年 | 7篇 |
2023年 | 20篇 |
2022年 | 27篇 |
2021年 | 41篇 |
2020年 | 54篇 |
2019年 | 49篇 |
2018年 | 49篇 |
2017年 | 57篇 |
2016年 | 65篇 |
2015年 | 59篇 |
2014年 | 74篇 |
2013年 | 46篇 |
2012年 | 72篇 |
2011年 | 79篇 |
2010年 | 61篇 |
2009年 | 62篇 |
2008年 | 79篇 |
2007年 | 91篇 |
2006年 | 75篇 |
2005年 | 40篇 |
2004年 | 36篇 |
2003年 | 39篇 |
2002年 | 27篇 |
2001年 | 22篇 |
2000年 | 33篇 |
1999年 | 32篇 |
1998年 | 39篇 |
1997年 | 12篇 |
1996年 | 12篇 |
1995年 | 9篇 |
1994年 | 16篇 |
1993年 | 3篇 |
1992年 | 7篇 |
1991年 | 10篇 |
1990年 | 7篇 |
1989年 | 3篇 |
1988年 | 6篇 |
1987年 | 1篇 |
1986年 | 1篇 |
排序方式: 共有1422条查询结果,搜索用时 0 毫秒
321.
322.
《Space Policy》2014,30(4):215-222
Although existing international instruments such as the Outer Space Treaty and Moon Agreement generally express sentiments for minimizing missions' extraterrestrial environmental impacts, they tend to be limited in scope, vague and generally unenforceable. There is no formal structure for assessing how and to what extent we affect those environments, no opportunity for public participation, no uniform protocol for documenting and registering the effects of our actions and no requirement to mitigate adverse impacts or take them into consideration in the decision-making process. Except for precautions limiting forward biological contamination and issues related to Earth satellites, environmental impact analysis, when done at all, remains focused on how missions affect the Earth and near-Earth environments, not how our actions affect the Moon, Mars, Europa, comets and other potential destinations. Extraterrestrial environmental impacts are potentially counterproductive to future space exploration, exploitation and scientific investigations. Clear, consistent and effective international protocols guiding a process for assessing such impacts are warranted. While instruments such as the US National Environmental Policy Act provide legally tested and efficient regulatory models that can guide impact assessment here on Earth, statutory legal frameworks may not work as well in the international environment of outer space. A proposal for industry-driven standards and an environmental code of conduct based, in part, on best management practices are offered for consideration. 相似文献
323.
324.
T. Hanada J.-C. Liou 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2008,41(7):1132-1137
This paper summarizes two new satellite impact experiments. The objective of the experiments was to investigate the outcome of low- and hyper-velocity impacts on two identical target satellites. The first experiment was performed at a low-velocity of 1.5 km/s using a 40-g aluminum alloy sphere. The second experiment was performed at a hyper-velocity of 4.4 km/s using a 4-g aluminum alloy sphere. The target satellites were 15 cm × 15 cm × 15 cm in size and 800 g in mass. The ratios of impact energy to target mass for the two experiments were approximately the same. The target satellites were completely fragmented in both experiments, although there were some differences in the characteristics of the fragments. The projectile of the low-velocity impact experiment was partially fragmented while the projectile of the hyper-velocity impact experiment was completely fragmented beyond recognition. To date, approximately 1500 fragments from each impact experiment have been collected for detailed analysis. Each piece has been weighed, measured, and analyzed based on the analytic method used in the NASA Standard Breakup Model (2000 revision). These fragments account for about 95% of the target mass for both impact experiments. Preliminary analysis results will be presented in this paper. 相似文献
325.
326.
非定常机匣处理对失速先兆波的抑制作用实验研究 总被引:6,自引:1,他引:5
非定常机匣处理在不影响效率的前提下可以明显提高压气机的稳定工作范围,针对这种通过改变斜槽和气室来调节壁面阻抗边界条件的新型处理机匣,从非定常角度,开展其对失速先兆波产生及发展的影响的实验研究.在压气机转子前缘附近沿圆周均匀布置八支高频响压力传感器,采集壁面动态压力信号,进行周向傅立叶分析(SFT)和功率谱密度分析(PSD),捕捉到旋转失速先兆波的出现和发展的动态细节,比较光壁和处理机匣两种情况的结果,证实了处理机匣并非阻止了失速先兆波的出现,而是有效的抑制了其非线性发展.非定常机匣处理改变了压气机系统的阻抗边界条件,能够在全过程中对低频扰动波进行有效的抑制,从而推迟旋转失速的发生,实现压气机的扩稳目的. 相似文献
327.
328.
首次采用网格分区的方法,对带有轴向斜槽式轮毂处理的压气机叶栅通道流场进行了数值模拟,分析了轴向斜槽式轮毂处理的扩稳机理以及它对压气机性能的影响的原因所在,进一步探讨轴向斜槽的几何参数的变化对其扩稳效果的影响.在计算中采用了非交错网格的SIMPLE算法,求解时均N-S方程,紊流模型采用基于RNG(重整化群)方法的K-ε紊流模型. 相似文献
329.
为保证系留气球平台在空投着陆中的安全,必须对其中的压力气瓶进行缓冲分析与实验。文章采用蜂窝纸板作为气瓶缓冲材料,采用LS-DYNA软件,并依据蜂窝纸板实际参数处理材料模型,仿真分析了在不同蜂窝纸板厚度、不同跌落速度和不同着陆姿态下的缓冲过程。根据仿真结果,设计了蜂窝纸板缓冲结构和加速度检测模块,采用吊车起吊跌落进行了实验验证。仿真分析和实验结果均表明,蜂窝纸板厚度为500mm,跌落速度低于10m/s时,气瓶缓冲后加速度低于20gn,可满足空投着陆应用要求。文章基于LS-DYNA的蜂窝纸板缓冲有限元分析是可行的,研究结果对于气瓶类装备的着陆缓冲结构设计有参考价值。 相似文献
330.