全文获取类型
收费全文 | 199篇 |
免费 | 46篇 |
国内免费 | 30篇 |
专业分类
航空 | 136篇 |
航天技术 | 64篇 |
综合类 | 31篇 |
航天 | 44篇 |
出版年
2024年 | 1篇 |
2023年 | 8篇 |
2022年 | 10篇 |
2021年 | 17篇 |
2020年 | 9篇 |
2019年 | 7篇 |
2018年 | 9篇 |
2017年 | 15篇 |
2016年 | 16篇 |
2015年 | 9篇 |
2014年 | 12篇 |
2013年 | 15篇 |
2012年 | 15篇 |
2011年 | 12篇 |
2010年 | 17篇 |
2009年 | 20篇 |
2008年 | 13篇 |
2007年 | 12篇 |
2006年 | 10篇 |
2005年 | 7篇 |
2004年 | 6篇 |
2003年 | 6篇 |
2002年 | 1篇 |
2001年 | 3篇 |
2000年 | 2篇 |
1999年 | 5篇 |
1998年 | 4篇 |
1997年 | 2篇 |
1996年 | 3篇 |
1995年 | 2篇 |
1994年 | 2篇 |
1993年 | 1篇 |
1992年 | 3篇 |
1987年 | 1篇 |
排序方式: 共有275条查询结果,搜索用时 15 毫秒
61.
62.
密集型阵列冲击射流换热特性实验 总被引:7,自引:2,他引:5
设计了多种不同几何参数的阵列射流冲击孔实验件,利用红外热像仪对其冲击冷却进行了热像显示实验,获得了冲击射流雷诺数和几何参数对局部对流换热特性的影响规律.结果表明:①对流换热系数随着射流雷诺数Rej的增加而逐渐增大;②随着孔间距的或者冲击间距的增大,冲击冷却的对流换热效果逐渐减弱;③当孔间距与孔径之比在3~5时,顺排阵列射流的强化换热效果优于叉排,而当孔间距与孔径之比为2时,在阵列射流上游叉排排布的强化换热效果优于顺排,而在下游则顺排排布的强化换热效果占优. 相似文献
63.
A theoretical model of ionospheric electric fields at mid- and low-latitudes is developed. In the geomagnetic dipolar coordinate system, the ionospheric dynamo equations were solved, and the ionospheric electric potential and electric field were derived respectively. Major parameters for the model inputs, such as the neutral winds, the densities and temperatures of electron, ions and neutrals, are obtained from empirical models. The global ionospheric electrical potential and field at mid- and low-latitudes derived from our model are largely in agreement with the results presented by other authors and the empirical model. Using our model, it is found that the diurnal component of the HWM93 wind mainly contributed to the formation of the vertical electric field, while the semidiurnal component mainly contributed to the zonal electric field. Finally, by adjustment of the input F region winds and conductivities, most discrepancies between our model and the empirical one can be eliminated, and it is proved that the F region dynamo is the most significant contribution to the electric fields. 相似文献
64.
The development of a fiber based laser architecture will enable novel applications in environments which have hitherto been impossible due to size, efficiency and power of traditional systems. Such a new architecture has been developed by the International Coherent Amplification Network (ICAN) project. Here we present an analysis of utilizing an ICAN laser for the purpose of tracking and de-orbiting hyper-velocity space debris. With an increasing number of new debris from collisions of active, derelict and new payloads in orbit, there is a growing danger of runaway debris impacts. Due to its compactness and efficiency, it is shown that space-based operation would be possible. For different design parameters such as fiber array size, it is shown that the kHz repetition rate and kW average power of ICAN would be sufficient to de-orbit small 1–10 cm debris within a single instance via laser ablation. 相似文献
65.
K.G. Simi C. Vineeth T.K. Pant 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
In this paper, through a case study, an attempt has been made to bring out the relationship between post noon E-region electric field and post sunset F-region vertical plasma drift on quiet time Counter Electrojet (CEJ) days. Study carried out using the data from a multi frequency HF Doppler Radar and Digital Ionosonde located over Trivandrum (8.5° N; 77° E; 0.5° N dip lat.) a geomagnetic dip equatorial station in India during quite time CEJ days of the years 2004 and 2006, revealed some interesting aspects of the E region electrodynamics and post sunset F region electrodynamics. It has been observed that, in contrast to the normal electrojet (EEJ) days, the Pre-Reversal Enhancement (PRE) is either weakened or inhibited on CEJ days and the field reversal takes place much earlier than that on a normal day. It is suggested that even after the effects of the field reversal ceases to show up in the ground magnetic data, the reversed field may persist and shows up as a decrease in the PRE experienced by the F-region. In other words, the study indicates that the EEJ associated electrodynamics have a significant role in controlling the PRE. 相似文献
66.
为提高空间碳纤维复合材料壳结构的导热能力,降低热控设计难度,并提高热控系统可靠性,设计了包含贴覆石墨高导热膜材料以及在外部包覆的多层隔热组件内增加高导热膜等在内的3种导热增强措施,分别按这3种方法制作了试件,并增加了对照组,进行了真空热试验。试验结果表明,贴覆石墨高导热膜材料的方法使碳纤维壳结构试件的当量导热系数增大了7倍,相较其他方法具有明显优势。若该方法与包覆含有高导热膜夹层的多层隔热组件的方法协同使用,可以取得更好的效果。 相似文献
67.
针对现有的去雾算法对彩色图像处理后会出现色彩畸变的问题,提出了基于Retinex算法和色度比的去雾算法,该算法在用Retinex算法进行图像恢复的过程中引入了原图像的色彩信息,改善了处理后的图像的色彩。 相似文献
68.
由于低轨道雷达卫星的飞行速度远快于飞机,波束同步技术是关系到星机双基地SAR能否具有实用价值的核心技术。已有文献中提出的基于收发波束指向控制的同步方法具有场景长度短、算法复杂等缺点。根据星机双基地SAR远发近收的特点,提出一种基于收发宽波束的波束同步方法。从信噪比、系统模糊性等方面对该方法进行量化论证。仿真结果验证了方法的可行性。与已有方法进行比较,结果表明,文中提出的方法能在方位分辨率相等的前提下获得更大的场景长度;而且由于无需进行波束指向控制,成像算法简单。 相似文献
69.
随着传统产业升级和新兴技术的发展,社会生产和生活对分米级、厘米级的实时精准定位需求日益凸显。低轨卫星轨道高度低、信号强度大、短时间内几何构型变化快,因此应用低轨卫星开展导航增强服务成为研究热点。低轨卫星的增强服务性能依赖于星座的快速组网和设计,低轨卫星星座构型、轨道高度、轨道倾角等是影响其覆盖性能和增强性能的关键因素。全面分析了低轨星座设计的关键要素,包括轨道高度、轨道倾角和单星覆盖性、地面人口密度、空间环境等,在此基础上设计了单构型和复合构型低轨导航增强星座,并进一步分析低轨星座的覆盖性能。结果显示:复合低轨导航增强星座可以实现对全球的连续覆盖,同时满足极地高密度覆盖和低纬度的连续覆盖需求,对北斗导航系统的增强效果明显。 相似文献
70.