全文获取类型
收费全文 | 7035篇 |
免费 | 1166篇 |
国内免费 | 1095篇 |
专业分类
航空 | 3863篇 |
航天技术 | 2462篇 |
综合类 | 635篇 |
航天 | 2336篇 |
出版年
2024年 | 53篇 |
2023年 | 174篇 |
2022年 | 239篇 |
2021年 | 364篇 |
2020年 | 373篇 |
2019年 | 501篇 |
2018年 | 646篇 |
2017年 | 466篇 |
2016年 | 450篇 |
2015年 | 435篇 |
2014年 | 419篇 |
2013年 | 366篇 |
2012年 | 518篇 |
2011年 | 571篇 |
2010年 | 399篇 |
2009年 | 391篇 |
2008年 | 431篇 |
2007年 | 400篇 |
2006年 | 397篇 |
2005年 | 284篇 |
2004年 | 218篇 |
2003年 | 163篇 |
2002年 | 115篇 |
2001年 | 149篇 |
2000年 | 102篇 |
1999年 | 82篇 |
1998年 | 94篇 |
1997年 | 76篇 |
1996年 | 69篇 |
1995年 | 77篇 |
1994年 | 86篇 |
1993年 | 35篇 |
1992年 | 30篇 |
1991年 | 31篇 |
1990年 | 38篇 |
1989年 | 19篇 |
1988年 | 22篇 |
1987年 | 7篇 |
1986年 | 2篇 |
1985年 | 1篇 |
1984年 | 2篇 |
1981年 | 1篇 |
排序方式: 共有9296条查询结果,搜索用时 15 毫秒
11.
本文首先分析了当前直升机在运用CAD/CAE/CAM技术进行研制中存在的一些问题,接着提供了解决的方法,介绍了PDM的概念、构成、主要功能。最后简述了PDM技术在直升机研制中的作用,以及企业在实施PDM当中应注意的一些问题。 相似文献
12.
经营机制创新是中小型外贸企业摆脱困境的必由之路。针对目前面临的主要问题,从外部环境及企业自身经营机制缺陷方面对中小型外贸企业生存环境进行分析,并从实现经营机制创新角度探讨改善现状的方法,力图找出中小型外贸企业经营机制创新的突破点。 相似文献
13.
A numerical procedure for the calculation of the transonic dip of airfoils in the time domain is presented. A viscous-inviscid aerodynamic interaction method is taken to calculate the unsteady aerodynamic loads. In the present case the integral boundary layer equations are coupled with the Transonic Small Disturbance (TSD) Potential Equation. The coupling between structural motion and aerodynamic loads is carried out using State Space equation. It is solved by State Transition Matrix technique. Results are presented for NACA 64A010 and NLR 7301 airfoils with structural data from Isogai and DLR, respectively. Comparisons show good agreement with other numerical results. Certain deviations of experimental data taken from literature need more insight in the detailed test conditions. 相似文献
14.
ected g 《桂林航天工业高等专科学校学报》2006,(2)
with primary goat embryonic fibroblast showed no difference from traditional feederlayer-based culture method used in mouse and human. The putative primary EG colonies were multilayer clumps ofcompact cel 相似文献
15.
16.
17.
本文对质量矩控制导弹的动力学方程简化和控制系统的设计进行了研究。详细阐述了所提出的控制方法,介绍了径向基单隐层神经网络进行误差补偿的算法原理,用Lyapunov理论证明了所采用方法的稳定性。在给出了质量矩导弹的六自由度动力学方程和简化后的方程后,用所提出的方法设计控制系统。通过仿真分析,得出了本文所提出的方法具有较好的误差补偿能力的结论。 相似文献
18.
Aiming at a 1-cm Orbit for Low Earth Orbiters: Reduced-Dynamic and Kinematic Precise Orbit Determination 总被引:1,自引:0,他引:1
The computation of high-accuracy orbits is a prerequisite for the success of Low Earth Orbiter (LEO) missions such as CHAMP,
GRACE and GOCE. The mission objectives of these satellites cannot be reached without computing orbits with an accuracy at
the few cm level. Such a level of accuracy might be achieved with the techniques of reduced-dynamic and kinematic precise
orbit determination (POD) assuming continuous Satellite-to-Satellite Tracking (SST) by the Global Positioning System (GPS).
Both techniques have reached a high level of maturity and have been successfully applied to missions in the past, for example
to TOPEX/POSEIDON (T/P), leading to (sub-)decimeter orbit accuracy. New LEO gravity missions are (to be) equipped with advanced
GPS receivers promising to provide very high quality SST observations thereby opening the possibility for computing cm-level
accuracy orbits. The computation of orbits at this accuracy level does not only require high-quality GPS receivers, but also
advanced and demanding observation preprocessing and correction algorithms. Moreover, sophisticated parameter estimation schemes
need to be adapted and extended to allow the computation of such orbits. Finally, reliable methods need to be employed for
assessing the orbit quality and providing feedback to the different processing steps in the orbit computation process.
This revised version was published online in August 2006 with corrections to the Cover Date. 相似文献
19.
Martin A. Lee 《Space Science Reviews》2007,130(1-4):221-229
Gradual solar energetic particle (SEP) events are evidently accelerated by coronal/interplanetary shocks driven by coronal
mass ejections. This talk addresses the different factors which determine the composition of the accelerated ions. The first
factor is the set of available seed populations including the solar wind core and suprathermal tail, remnant impulsive events
from preceding solar flares, and remnant gradual events. The second factor is the fractionation of the seed ions by the injection
process, that is, what fraction of the ions are extracted by the shock to participate in diffusive shock acceleration. Injection
is a controversial topic since it depends on the detailed electromagnetic structure of the shock transition and the transport
of ions in these structured fields, both of which are not well understood or determined theoretically. The third factor is
fractionation during the acceleration process, due to the dependence of ion transport in the turbulent electromagnetic fields
adjacent to the shock on the mass/charge ratio. Of crucial importance in the last two factors is the magnetic obliquity of
the shock. The form of the proton-excited hydromagnetic wave spectrum is also important. Finally, more subtle effects on ion
composition arise from the superposition of ion contributions over the time history of the shock along the observer’s magnetic
flux tube, and the sequence of flux tubes sampled by the observer. 相似文献
20.
Several automated optical telescopes have been setup at appropriate longitudes around the globe to study earthshine variations
and asteroseismology. The first telescope has been setup at Teide Observatory, Tenerife, Spain in October 2004. The intensity
of earthshine relates to the average of Earth’s albedo, and in turn relates to the global temperature of the Earth. A global
network is necessary because each site can measure the earthshine reflected from only a part of the Earth. The network will
also be used for asteroseismology study. It can measure photometric variations of pulsating stars. The long-term and continuous
measurements allow the accurate determination of mode frequencies of stellar pulsations, which provides information on the
properties of stellar interior. 相似文献