全文获取类型
收费全文 | 217篇 |
免费 | 47篇 |
国内免费 | 28篇 |
专业分类
航空 | 159篇 |
航天技术 | 44篇 |
综合类 | 16篇 |
航天 | 73篇 |
出版年
2024年 | 6篇 |
2023年 | 7篇 |
2022年 | 10篇 |
2021年 | 17篇 |
2020年 | 10篇 |
2019年 | 8篇 |
2018年 | 5篇 |
2017年 | 9篇 |
2016年 | 22篇 |
2015年 | 7篇 |
2014年 | 17篇 |
2013年 | 6篇 |
2012年 | 10篇 |
2011年 | 21篇 |
2010年 | 13篇 |
2009年 | 17篇 |
2008年 | 17篇 |
2007年 | 21篇 |
2006年 | 11篇 |
2005年 | 9篇 |
2004年 | 11篇 |
2003年 | 11篇 |
2002年 | 6篇 |
2001年 | 4篇 |
2000年 | 1篇 |
1999年 | 5篇 |
1997年 | 1篇 |
1996年 | 2篇 |
1995年 | 3篇 |
1994年 | 2篇 |
1993年 | 1篇 |
1991年 | 1篇 |
1990年 | 1篇 |
排序方式: 共有292条查询结果,搜索用时 495 毫秒
241.
根据在相同的环境温度下和不同环境温度下对船体轴系部位同一材料、相同结构的多个目标点进行反复测量,观察全站仪测量数据的变化,分析环境温度变化引起的误差情况,为船舶精度建造工艺研究提供可靠的数据支撑。 相似文献
242.
Jianguo Yan Oliver Baur Li Fei Ping Jinsong 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2013
As has been demonstrated recently, inter-satellite Ka-band tracking data collected by the GRAIL (Gravity Recovery And Interior Laboratory) spacecraft have the potential to improve the resolution and accuracy of the lunar gravity field by several orders of magnitude compared to previous models. By means of a series of simulation studies, here we investigate the contribution of inter-satellite ranging for the recovery of the Moon’s gravitational features; the evaluation of results is made against findings from ground-based Doppler tracking. For this purpose we make use of classical dynamic orbit determination, supported by the analysis of satellite-to-satellite tracking observations. This study sheds particularly light on the influence of the angular distance between the two satellites, solar radiation modeling and the co-estimation of the lunar Love number k2. The quality of the obtained results is assessed by gravity field power spectra, gravity anomalies and precision orbit determination. We expect our simulation results to be supportive for the processing of real GRAIL data. 相似文献
243.
244.
《中国航空学报》2021,34(2):620-628
A kind of interlaminar film with carbon nanotubes inserted into polyether ketone with cardo was used for lightning strike protection of composite laminates. The distribution of the interlaminar film was investigated by experimental and numerical methods. Artificial lightning strike tests were conducted for 12-film carbon nanotube and traditional surface silver coating protected specimens. Then corresponding finite element models (FEMs) were established to analyze the lightning strike effect and validated by the experimental results. Based on the FEMs, the number, distribution and thickness of interlaminar film were investigated in order to obtain equivalent protection effect with the traditional surface silver coating. The results show that only the first two layers were damaged for the surface silver coating protected specimen, while 5 layers were ablated for the 12-film protected specimen. Lightning strike damage area of the laminate protected with 5-film carbon nanotube is almost the same as that of the laminate protected with 12-film carbon nanotube. Compared with traditional surface silver coating protection, one film protection with thickness of 360 μm can make the laminate to obtain equivalent damage depth, 54.8% smaller damage area and 58% less additional weight. And reparability of the laminate is better than that of the laminate protected with 5 interlaminar films. 相似文献
245.
246.
247.
248.
智能发动机是1种先进的新概念航空发动机,是美国IHPTET计划及其后继计划——VAATE计划最核心的内容。对智能发动机,简述了其概念和特点,重点综述了其关键技术和其智能状态监视与故障诊断技术。 相似文献
249.
通过雷电模拟,对复合材料层合板试样进行雷击损伤试验。基于热扩散原理,针对不同的雷击试验件,采用波形为长脉冲形式的瞬态热激励方式对雷击损伤进行红外热成像检测,并对不同时刻的检测结果进行分析、比较,对缺陷轮廓进行界定,对结果进行定量测量。检测结果表明,无论是否对碳纤维复合材料表面进行防护,瞬态红外热成像方法均能够有效检测出雷击后的内部分层损伤,可对损伤的严重程度进行有效区分,能够对缺陷尺寸、面积进行准确测量。 相似文献
250.
针对传统火力分配模型容易造成资源浪费的问题,将火力单元以组为单位,以最大化杀伤概率为目标,构建一种具有多次拦截时机的动态火力分配模型;考虑到组内火力单元复合打击的情况,使用Kuhn-Munkres算法,优先将目标分配给复合打击效果大的目标;在此基础之上,设计了一种基于遗传算法(GA)的Anytime算法,引入了元级控制,提出一种任意时刻算法停机时刻的判定方法;仿真实验验证了模型优越性以及算法的合理性,对火力分配任意时刻算法使用元级控制可以有效提高解的效用。 相似文献