全文获取类型
收费全文 | 204篇 |
免费 | 53篇 |
国内免费 | 50篇 |
专业分类
航空 | 149篇 |
航天技术 | 64篇 |
综合类 | 23篇 |
航天 | 71篇 |
出版年
2024年 | 1篇 |
2023年 | 5篇 |
2022年 | 3篇 |
2021年 | 12篇 |
2020年 | 13篇 |
2019年 | 14篇 |
2018年 | 13篇 |
2017年 | 14篇 |
2016年 | 15篇 |
2015年 | 9篇 |
2014年 | 10篇 |
2013年 | 11篇 |
2012年 | 14篇 |
2011年 | 21篇 |
2010年 | 18篇 |
2009年 | 18篇 |
2008年 | 12篇 |
2007年 | 12篇 |
2006年 | 11篇 |
2005年 | 12篇 |
2004年 | 6篇 |
2003年 | 11篇 |
2002年 | 12篇 |
2001年 | 9篇 |
2000年 | 6篇 |
1999年 | 3篇 |
1998年 | 1篇 |
1997年 | 5篇 |
1995年 | 2篇 |
1994年 | 1篇 |
1993年 | 1篇 |
1992年 | 2篇 |
1991年 | 4篇 |
1990年 | 2篇 |
1989年 | 2篇 |
1988年 | 1篇 |
1987年 | 1篇 |
排序方式: 共有307条查询结果,搜索用时 390 毫秒
241.
M. Arslan Tariq Munawar Shah M. Hernández-Pajares Talat Iqbal 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2019,63(7):2088-2099
The dual-frequency satellite-based measurements from Global Positioning System (GPS) may provide feasible ways of studying and potentially detecting of earthquake (EQ) related anomalies in the ionosphere. In this paper, GPS based Total Electron Content (TEC) data are studied for three major M?>?7.0 EQs in Nepal and Iran-Iraq border during 2015–2017 by implementing statistical procedures on temporal and spatial scale. Previous studies presented different time interval of pre-seismic ionospheric anomalies, however, this study showed that EQs ionospheric precursors may occur within 10?days. Furthermore, the ionospheric anomalies on the suspected day occurred during UT?=?08:00–12:00?h before the main shock. The Global Ionospheric Map TEC (GIM-TEC) data retrieved over the epicenter of M7.8 (Nepal EQ) showed a significant increase of 6 TECU on April 24, 2015 (one day before the main shock), which is recorded by the ground GPS station data of Islamabad (station lies within the EQ preparation zone). Furthermore, the spatial GIM-TEC result imply significant anomalies over the epicenter during the time interval between UT?=?08:00–12:00?h (LT?=?13:00–17:00). For M7.3 (Nepal EQ), the TEC anomalies were detected on May 10, 2015 (2?days before the event) in the temporal data. The spatial TEC data imply the huge clouds over the epicenter at about UT?=?08:00–12:00?h on May 10, 2015, that may be associated with this EQ in the quiet geomagnetic storm conditions. Similarly, temporal and spatial TEC showed anomaly on November 3, 2017, during UT?=?08:00–12:00 (9?days before the Iran-Iraq border EQ) after implementing the statistical method on it. Conversely, there exists a short-term but low magnitude TEC anomaly synchronized with a geomagnetic storm on November 7–8, 2017 (4 to 5?days prior to M7.3 Iran-Iraq border EQ). The diurnal and hourly GIM-TEC and VTEC data also imply the execution of ionospheric anomalies within 10?days prior to all events. All these positive anomalies in TEC may be due to the existence of a huge energy from the epicenter during the EQ preparation period. 相似文献
242.
243.
244.
245.
A study of micrometeoroid and orbital debris (MMOD) long-term effects on solar cell samples of solar panels returned from the space station MIR has been carried out. Five samples from the solar array, which spent over 10 years in space, have been studied with the help of optical microscopes with magnification up to 1000. Craters with dimensions as small as 1m were registered. Additional large impact features were investigated by observing a large number of cells (150) with an optical microscope of small magnification. The aim of the study was to define morphological and statistical characteristics of samples surface damages as well as the extent of surface erosion caused by MMOD impacts. The results of statistical analysis of the data obtained in this study are shown to correlate with the experimental data obtained in the Hubble Telescope solar panel return experiment, and MMOD flux estimations are in good agreement with modern MMOD models. The relative surface area damaged by impacts of small size (1–100m) MMOD particles is estimated to be 0.01%, while the relative surface area of large impact features (greater than 0.1mm) is estimated to be 0.045%. 相似文献
246.
国产CCM40J-6K高模碳纤维基板的空间高低温热循环耐受性是决定其是否可以大规模应用于空间太阳电池板的关键因素,必须解决交变热环境下的面板与电池电路的匹配性和长寿命问题。本文以国产CCM40J-6K高模碳纤维/环氧复合材料的太阳电池板为研究对象,开展了热循环环境适应性试验研究,分别从国产和进口碳纤维基板适应高低温交变能力对比、国产碳纤维基板铺设电池电路后适应热环境能力以及电池板在轨寿命等3个方面进行测试试验。结果表明:国产碳纤维CCM40J-6K所构成的电池板综合性能与进口M40JB-6K相当,CCM40J-6K基板与三结砷化镓电池片匹配性良好,国产碳纤维电池板经疲劳热循环后的开路电压和短路电流的变化率分别为0.55%和0.24%,太阳电池片和玻璃盖片外观完好无损,太阳电池电路与基板聚酰亚胺面保持绝缘,且碳纤维表面无脱粘现象。说明国产碳纤维CCM40J-6K能够应用于太阳电池板研制。 相似文献
247.
248.
249.
本文介绍进口流场畸变对发动机稳定性的影响.文章针对某型双轴涡喷发动机在湍流型动态畸变流场条件下压气机喘振放炮的实例,重点分析了该发动机在高空台喘振放炮的原因及其排除故障的方法.增设气动格栅和收敛段整流装置可使进口流场较为均匀,使涡喷发动机在高空台地面进气流场下工作稳定可靠. 相似文献
250.
采用DSMC/EPSM混合算法,研究了带有侧向喷流的复杂外形高超声速飞行器稀薄区和连续区三维混合流场的干扰特性。采用一种飞行器物面网格与DSMC计算域网格分别标识的方法,通过判断模拟分子与表面碰撞来完成飞行器物面网格与DSMC计算域网格间的信息传递和信息存贮,对于复杂外形飞行器的精确描述的物面网格不需做进一步处理,直接应用于不依赖于飞行器外形的DSMC计算的通用子程序中。引入碰撞数做为混合参数,对流动区域进行划分,并通过网格中碰撞数的统计和处理,有效地将DSMC和EPSM方法结合在一起。仿真计算了三维复杂外形飞行器带喷流流场压力、热流分布量,飞行器表面气动力、气动力矩和气动热参数,对喷流与高超声速空气绕流相互作用以及它们与物面之间的相互扰动进行了分析,证明了采用的方案和技术的有效性。 相似文献