全文获取类型
收费全文 | 14502篇 |
免费 | 2530篇 |
国内免费 | 2713篇 |
专业分类
航空 | 9021篇 |
航天技术 | 3863篇 |
综合类 | 2420篇 |
航天 | 4441篇 |
出版年
2024年 | 37篇 |
2023年 | 105篇 |
2022年 | 284篇 |
2021年 | 346篇 |
2020年 | 437篇 |
2019年 | 260篇 |
2018年 | 300篇 |
2017年 | 301篇 |
2016年 | 289篇 |
2015年 | 545篇 |
2014年 | 822篇 |
2013年 | 846篇 |
2012年 | 977篇 |
2011年 | 1041篇 |
2010年 | 1165篇 |
2009年 | 1183篇 |
2008年 | 1074篇 |
2007年 | 994篇 |
2006年 | 863篇 |
2005年 | 705篇 |
2004年 | 515篇 |
2003年 | 430篇 |
2002年 | 465篇 |
2001年 | 506篇 |
2000年 | 521篇 |
1999年 | 650篇 |
1998年 | 613篇 |
1997年 | 500篇 |
1996年 | 458篇 |
1995年 | 364篇 |
1994年 | 400篇 |
1993年 | 339篇 |
1992年 | 310篇 |
1991年 | 265篇 |
1990年 | 225篇 |
1989年 | 193篇 |
1988年 | 141篇 |
1987年 | 111篇 |
1986年 | 60篇 |
1985年 | 25篇 |
1984年 | 18篇 |
1983年 | 16篇 |
1982年 | 17篇 |
1981年 | 9篇 |
1980年 | 4篇 |
1974年 | 3篇 |
1973年 | 3篇 |
1966年 | 1篇 |
1965年 | 4篇 |
1900年 | 1篇 |
排序方式: 共有10000条查询结果,搜索用时 156 毫秒
1.
客流密度是影响地铁列车客室内热舒适性环境的重要因素,传统的地铁列车客室温度控制主要是根据UIC-553标准,以室内外温差作为控制核心.本文通过构建全尺寸地铁列车客室-乘客-空调送风耦合的一体化模型,利用实车试验与数值模拟相结合的方法,对地铁列车客室内的热舒适性展开研究.探讨客流密度对地铁列车客室内热舒适环境的影响规律以及不同客流密度下客室平均温度与空调送风温度之间的关系,得到了不同客流密度下能满足人体热舒适性体验的空调送风温度,提出了一种基于客流密度的地铁列车空调夏季送风温度控制模型. 相似文献
2.
Yi Wei Qingjun Li Fangnuan Xu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2021,67(1):393-400
A new orbit-attitude-vibration coupled dynamic model of the tethered solar power satellite (Tethered SPS) is established based on absolute nodal coordinate formulation. The Hamilton’s equation of the system is derived by introducing generalized momentum through Legendre transformation. The correctness of the proposed model is verified by an example. The dynamic characteristics of the Tethered SPS are studied using the symplectic Runge-Kutta method. Simulation results show that the orbital radius and the total energy of the system are well preserved. The attitude of the system is unstable when the mass of the bus system is small. However, the attitude stability is dependent on some other parameters of the system, which requires further studies. It is also found that the average tether force/deformation can be roughly estimated by simplifying the solar panel as a particle. The proposed model can be used to study the orbit-attitude-vibration coupled dynamics and control problems. 相似文献
3.
Yongjie Ding Jia Boyang Hezhi Sun Liqiu Wei Wuji Peng Peng Li Daren Yu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(3):837-843
Discharge characteristics of a non-wall-loss Hall thruster were studied under different channel lengths using a design based on pushing a magnetic field through a double permanent magnet ring. The effect of different magnetic field intensities and channel lengths on ionization, efficiency, and plume divergence angle were studied. The experimental results show that propellant utilization is improved for optimal matching between the magnetic field and channel length. While matching the magnetic field and channel length, the ionization position of the neutral gas changes. The ion flow is effectively controlled, allowing the thrust force, specific impulse, and efficiency to be improved. Our study shows that the channel length is an important design parameter to consider for improving the performance of non-wall-loss Hall thrusters. 相似文献
4.
5.
The hierarchical porous N/O co-functionalized carbon(HPNOC)was scalably prepared by using the lowcost and renewable blighted grains as the raw material coupled with mild KHCO_3 activation for electrochemical capacitors(ECs).The elemental N was in situ doped in the obtained HPNOC without any N-containing additives.Remarkably,the obtained HPNOC was endowed with a large specific surface area(about 2 624m~2·g~(-1)),high pore volume(about 1.35cm~3·g~(-1)),as well as high-content N/O functionalization(about 1.9%(in atom)N and about 10.2%(in atom)O.Furthermore,the as-resulted HPNOC electrode with a high mass loading of 5mg·cm~(-2 )exhibited competitive gravimetric capacitances of about 373.6F·g~(-1 )at 0.5A·g~(-1),and even about 260.4F·g~(-1 )at a high rate of 10A·g~(-1);superior capacitance retention of about 98.8%at 1A·g~(-1 )over 10 000consecutive cycles;and high specific energy of about 9.6W·h·kg~(-1 )at a power of 500W·kg~(-1),when evaluated as a promising electrode in 6mol KOH for advanced electrochemical supercapacitors.More encouragingly,the green synthetic strategy we developed holds a huge promise in generalizing for other biomass-derived carbon materials for versatile energy-related applications. 相似文献
6.
Yu Jiang Hexi Baoyin Hengnian Li 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2018,61(5):1371-1385
We investigate the orbital stability close to the unique L4-point Jupiter binary Trojan asteroid 624 Hektor. The gravitational potential of 624 Hektor is calculated using the polyhedron model with observational data of 2038 faces and 1021 vertexes. Previous studies have presented three different density values for 624 Hektor. The equilibrium points in the gravitational potential of 624 Hektor with different density values have been studied in detail. There are five equilibrium points in the gravitational potential of 624 Hektor no matter the density value. The positions, Jacobian, eigenvalues, topological cases, stability, as well as the Hessian matrix of the equilibrium points are investigated. For the three different density values the number, topological cases, and the stability of the equilibrium points with different density values are the same. However, the positions of the equilibrium points vary with the density value of the asteroid 624 Hektor. The outer equilibrium points move away from the asteroid’s mass center when the density increases, and the inner equilibrium point moves close to the asteroid’s mass center when the density increases. There exist unstable periodic orbits near the surface of 624 Hektor. We calculated an orbit near the primary’s equatorial plane of this binary Trojan asteroid; the results indicate that the orbit remains stable after 28.8375?d. 相似文献
7.
针对光学遥感卫星飞轮微振动引起的成像质量下降问题,设计了一种组合隔振装置,并采用仿真分析与实验测试相结合的方法对隔振方案设计的合理性进行验证。首先,将测量的飞轮扰振数据引入光学卫星的有限元模型中,计算出飞轮扰振对光学相机的像素偏移影响;其次,设计了组合隔振方案并基于有限元方法对其隔振效果进行验证;最后,搭建了光学成像微振动实验测试平台,对不同转速下飞轮微振动造成的像素偏移影响进行精确测量。实验结果表明,组合隔振装置对300 Hz以上高频段飞轮扰振有较大衰减作用,最大像素偏移降到0.01个像素以下,隔振效率达到80%以上;通过对比可知,实验测试与仿真计算得到的像素偏移结果在低频段一次谐波响应及模态响应表现出较好一致性,但在高频段二者存在一定偏差。 相似文献
8.
10.
L O Bjorn S Widell T Wang 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2002,30(6):1557-1562
Plants have evolved under the influence of UV-B radiation and have acquired systems for monitoring it and investing appropriate resources for protection against it, i.e., filters, quenchers of radicals and reactive oxygen species, and repair systems. An hypothesis for how plants monitor radiation has been presented. 相似文献