全文获取类型
收费全文 | 1941篇 |
免费 | 389篇 |
国内免费 | 292篇 |
专业分类
航空 | 1713篇 |
航天技术 | 261篇 |
综合类 | 365篇 |
航天 | 283篇 |
出版年
2024年 | 3篇 |
2023年 | 24篇 |
2022年 | 66篇 |
2021年 | 87篇 |
2020年 | 106篇 |
2019年 | 99篇 |
2018年 | 78篇 |
2017年 | 105篇 |
2016年 | 121篇 |
2015年 | 116篇 |
2014年 | 141篇 |
2013年 | 131篇 |
2012年 | 140篇 |
2011年 | 160篇 |
2010年 | 145篇 |
2009年 | 127篇 |
2008年 | 98篇 |
2007年 | 109篇 |
2006年 | 97篇 |
2005年 | 86篇 |
2004年 | 67篇 |
2003年 | 51篇 |
2002年 | 58篇 |
2001年 | 48篇 |
2000年 | 37篇 |
1999年 | 28篇 |
1998年 | 25篇 |
1997年 | 41篇 |
1996年 | 39篇 |
1995年 | 23篇 |
1994年 | 26篇 |
1993年 | 40篇 |
1992年 | 31篇 |
1991年 | 14篇 |
1990年 | 18篇 |
1989年 | 19篇 |
1988年 | 11篇 |
1987年 | 5篇 |
1986年 | 2篇 |
排序方式: 共有2622条查询结果,搜索用时 109 毫秒
81.
载人航天器空气环境参数控制非定常仿真分析 总被引:2,自引:0,他引:2
为支持乘员在轨驻留,载人航天器需通过空气环境控制系统将众多设计参数和空气环境参数控制在指标范围内。文章建立了一种载人航天器空气环境非定常控制仿真分析模型,包括舱体模块、航天员模块、舱压控制模块、温湿度控制模块以及CO2净化模块。利用该模型分析了载人航天器空气环境参数随乘员代谢水平的非定常变化趋势,并评估了控制系统的工作性能。结果表明:乘员代谢水平变化对空气环境参数有显著影响,通过调节控制系统运行参数可将各空气参数控制在有效指标范围内。人区温度与O2分压、CO2分压和人区湿度有密切的影响关系,不可孤立地进行分析。为载人航天器空气环境参数控制系统的设计和流程改进提供了依据。 相似文献
82.
本文对航空火箭弹射座椅弹射筒内筒钢球收压技术要求、难点进行了工艺分析;介绍了钢球收压工艺技术难点、检测方法及注意事项等,在工艺技术研究及设计过程中取得了一定的技术积累,具有良好的借鉴、推广应用意义。 相似文献
83.
在保证面积不变的情况下,选取不同的长轴、短轴,对波瓣混合器进行椭圆形切扇修形,研究切口深度与宽度对波瓣混合器掺混性能的影响规律。使用商用 CFD 软件对流场进行数值模拟。结果显示,对波瓣侧壁进行切扇处理会加强流向涡的强度,切扇越深,流向涡强度越大;切扇波瓣流向涡的耗散速率要大于基准波瓣混合器的流向涡耗散速率,预示着更为高效的掺混;引射系数与切口深度成正比,而总压恢复系数与切口深度成反比。考察了两种衡量热混合效率的模型并对其信度进行了比较,发现在 x =0.4 m 之前切扇可以提高热混合效率,而在 x =0.4 m 之后,基准波瓣混合器热混合效率要大于切扇波瓣混合器。 相似文献
84.
85.
Panagiotis K. Marhavilas 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2012
The analysis of energetic particles and magnetic field measurements from the Ulysses spacecraft has shown that in a series of events, the energy density contained in the suprathermal tail particle distribution is comparable to or larger than that of the magnetic field, creating conditions of high-beta plasma. In this work we analyze periods of high-beta suprathermal plasma occurrences (βep > 1) in interplanetary space, using the ratio (βep) of the energetic particle (20 keV to ∼5 MeV) and magnetic field energy densities from measurements covering the entire Ulysses mission lifetime (1990–2009) in order to reveal new or to reconfirm some recently defined interesting characteristics. The main key-results of the work are summarized as follows: (i) we verify that high-beta events are detected within well identified regions corresponding mainly to the vicinity of shock surfaces and magnetic structures, and associated with energetic particle intensity enhancements due to (a) reacceleration at shock-fronts and (b) unusually large magnetic field depressions. (ii) We define three considerable features for the high-beta events, concentrated on the next points: (a) there is an appreciable solar-activity influence on the high-beta events, during the maximum and middle solar-cycle phase, (b) the annual peak magnitude and the number of occurrences of high events are well correlated with the sunspot number, (c) the high-beta suprathermal plasma events present a spatial distribution in heliographic latitudes (HL) up to ∼±80°, and a specific important concentration on the low (−25° ? HL < −6°, 6° < HL ? 25°) and median (−45° ? HL < −25°, 25° < HL ? 45°) latitudes. We also reconfirm by a statistical analysis the results of Marhavilas and Sarris (2011), that the high-beta suprathermal plasma (βep > 1) events are characterized by a very large parameter βep (up to 1732.5), a great total duration (406 days) and a large percentage of the Ulysses-mission lifetime (which is equal to 6.34% of the total duration with usable measurements, and 11.3% of the duration in presence of suprathermal particles events). 相似文献
86.
油液含气量对液压系统的影响 总被引:2,自引:0,他引:2
飞机液压系统油液的含气量,空气进入飞机液压系统的形式以及飞机液压系统油液中的空气对飞机液压系统的影响,慢慢被国内外从事液压系统研制人们所重视,在国内,一些大专院校和液压技术研究机构正着手研究液压系统中这些问题。一个好的液压系统,它的抗故障能力是较强的,但是,设计中忽视某些问题,则容易产生这样、那样的故障,甚至使液压系统造成灾难性后果,应引起我们重视。 相似文献
87.
夏春林 《南京航空航天大学学报》1997,29(1):90-95
用数值方法求解绕过两圆柱的对流传热问题。贝克列数在0-50的范围内,了四种不同间距时的传热情况。从中发现两圆柱的传热特性相互有影响,这种影响随意距变化很敏感,两圆柱中任一个的平均谢尔特数总是小于单个圆柱的。并给出了简化计算的条件与公式。 相似文献
88.
89.
A.A. Arellano-Baeza R.V. García M. Trejo-Soto A. Martinez Bringas 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
Mexico is one of the most volcanically active regions in North America. Volcanic activity in central Mexico is associated with the subduction of the Cocos and Rivera plates beneath the North American plate. Periods of enhanced microseismic activity, associated with the volcanic activity of the Popocatépetl volcano are compared with periods, during which the microseismic activity was low. We detected systematical changes in the number of lineaments, associated with the microseismic activity due to lineament analysis of a temporal sequence of high resolution satellite images of the Popocatépetl volcano, provided by the ASTER/VNIR instrument. The Lineament Extraction and Stripes Statistic Analysis (LESSA) software package was used for the lineament extraction. In the future it would allow develop a methodology for detection of possible elevation of pressure in volcano edifice. 相似文献
90.
L. Anselmo C. Pardini 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2009
A large set of simulations, including all the relevant perturbations, was carried out to investigate the long-term dynamical evolution of fictitious high area-to-mass ratio (A/M) objects released, with a negligible velocity variation, in each of the six orbital planes used by Global Positioning System (GPS) satellites. As with similar objects discovered in near synchronous trajectories, long lifetime orbits, with mean motions of about 2 revolutions per day, were found possible for debris characterized by extremely high area-to-mass ratios. Often the lifetime exceeds 100 years up to A/M ∼ 45 m2/kg, decreasing rapidly to a few months above such a threshold. However, the details of the evolution, which are conditioned by the complex interplay of solar radiation pressure and geopotential plus luni-solar resonances, depend on the initial conditions. Different behaviors are thus possible. In any case, objects like those discovered in synchronous orbits, with A/M as high as 20–40 m2/kg, could also survive in this orbital regime, with semi-major axes close to the semi-synchronous values, with maximum eccentricities between 0.3 and 0.7, and with significant orbit pole precessions (faster and wider for increasing values of A/M), leading to inclinations between 30° and more than 90°. 相似文献