首页 | 本学科首页   官方微博 | 高级检索  
文章检索
  按 检索   检索词:      
出版年份:   被引次数:   他引次数: 提示:输入*表示无穷大
  收费全文   5774篇
  免费   2篇
  国内免费   11篇
航空   3069篇
航天技术   1549篇
综合类   181篇
航天   988篇
  2021年   29篇
  2018年   188篇
  2017年   147篇
  2016年   71篇
  2015年   33篇
  2014年   73篇
  2013年   100篇
  2012年   145篇
  2011年   279篇
  2010年   218篇
  2009年   299篇
  2008年   273篇
  2007年   240篇
  2006年   88篇
  2005年   135篇
  2004年   127篇
  2003年   139篇
  2002年   179篇
  2001年   200篇
  2000年   93篇
  1999年   123篇
  1998年   153篇
  1997年   99篇
  1996年   138篇
  1995年   168篇
  1994年   146篇
  1993年   99篇
  1992年   124篇
  1991年   57篇
  1990年   63篇
  1989年   125篇
  1988年   58篇
  1987年   60篇
  1986年   51篇
  1985年   152篇
  1984年   120篇
  1983年   108篇
  1982年   117篇
  1981年   153篇
  1980年   56篇
  1979年   46篇
  1978年   57篇
  1977年   37篇
  1976年   40篇
  1975年   48篇
  1974年   39篇
  1972年   49篇
  1971年   47篇
  1970年   30篇
  1969年   33篇
排序方式: 共有5787条查询结果,搜索用时 15 毫秒
401.
An Exact Trajectory Solution from Doppler Shift Measurements   总被引:2,自引:0,他引:2  
Three radar Doppler shift measurements are sufficient to determine the range and velocity, and the angle between them, of a target in uniform rectilinear motion. A solution using derivative approximations has recently appeared. An exact solution in terms of the original measurements is presented here.  相似文献   
402.
403.
It is shown that the common series resonant power converter is subject to a low frequency oscillation that can lead to the loss of cyclic stability. This oscillation is caused by a low frequency resonant circuit formed by the normal L and C components in series with the magnetizing inductance of the output transformer. Three methods for eliminating this oscillation are presented and analyzed. One of these methods requires a change in the circuit topology during the resonance cycle. This requires a new set of steady state equations which are derived and presented in a normalized form. Experimental results are included which demonstrate the nature of the low frequency oscillation before cyclic stability is lost.  相似文献   
404.
405.
From a short observation of GX 5-1 with EXOSAT we have derived information on spectral and temporal behaviour in the energy range 1–20 keV. The source was found to be variable on time scales from 10 s to 1 h. Describing the spectrum one is forced to assume at least two spectral components. The best fit is reached using a spectrum composed of two blackbody functions with typical temperatures 1 keV and 2 keV, corresponding to apparent blackbody radii of 43 km and 11 km, respectively (for a distance of 10 kpc). With respect to the hot component there is evidence for variability in temperature as well as in apparent blackbody radius. No periodic variability has been found over the period range 0.25 s to 2000 s. There is no evidence for an iron emission line.  相似文献   
406.
We present optical spectroscopy and photometry of 4U 1258-61 obtained over the course of six years. Evidence for the evolution of a circumstellar envelope throughout the course of the observations is presented.  相似文献   
407.
EXOSAT observed LMC X-4 on November 17/19, 1983 for one 1.4 day binary period during the high state of the 30.5 day cycle. An eclipse with sharp ingress and slow egress was detected with an eclipse angle of 27.1±1.0 dgr. In the medium energy experiment the source showed a hard power law spectrum. Outside eclipse the source was remarkably constant and only one flare was detected on November 17 at 19 UT lasting for about 1 h. The energy spectrum of the source softens considerably during that time and shows an emission line of cold iron. 13.5 sec pulsations are strongly present during the flare and have also been detected during the quiescent period and during several 1 min flares in another EXOSAT LMC X-4 observation on November 22, 1983. A pulse delay time analysis results in the determination of the pulse period (13.5019±0.0002) s and of the semimajor axis of the orbit of the X-ray star (26.0±0.6) It-sec. These results, together with other available information on LMC X-4, allowed to improve the binary parameters. The mass of the neutron star is found to be 1.34 ±0.44 0.48 Mo (95% confidence errors).  相似文献   
408.
The results of a previous discrete-time model of the series resonant dc-dc converter are reviewed and from these a small signal dynamic model is derived. This model is valid for low frequencies and is based on the modulation of the diode conduction angle for control. The basic converter is modeled separately from its output filter to facilitate the use of these results for design purposes. Experimental results are presented.  相似文献   
409.
湿热对单向复合材料层合板Ⅱ型分层特性的影响   总被引:1,自引:0,他引:1  
利用横向裂纹拉伸试验模型(Transverse Crack Tension-tension Test),在3种湿热环境(室温、85℃和85℃/95%RH)条件下,对2种单向碳纤维增强树脂基复合材料(T300/QY8911和HTA/6376)层合板的Ⅱ型分层特性进行了试验研究。结果表明湿热环境导致复合材料层间断裂韧性降低,引起Ⅱ型应变能释放率门槛值显着下降,裂纹扩展速率大大提高,温度的影响较湿度更为明显。利用电镜(SEM)对试样分层表面进行了检测,湿度对断面特征无明显的影响。  相似文献   
410.
Beers  T.C.  Rossi  S.  Norris  J.E.  Ryan  S.G.  Molaro  P.  Rebolo  R. 《Space Science Reviews》1998,84(1-2):139-144
Ongoing spectroscopy and photometry of stars selected in the HK objective-prism/interference-filter survey of Beers and colleagues has resulted in the identification of many hundreds of additional stars in the halo (and possibly the thick disk) of the Galaxy with abundances [Fe/H] -2.0. A new calibration of the technique for estimation of metal abundance based on a CaII K index as a function of broadband B - V color is applied to obtain metallicities for stars observed with the SSO 2.3m and INT 2.5m telescopes. This new data is combined with other samples of extremely metal-deficient stars (Ryan and Norris, 1991a; Beers et al., 1992; Carney et al., 1994) to form a large database of objects of low metallicity. The combined sample is examined and compared with expectations derived from a Simple Model of Galactic chemical evolution. There appears to be a statistically-significant deficit of stars more metal-weak than [Fe/H] = -3.0. An abundance of [Fe/H] -4.0 can be taken as the low-metallicity limit for presently-observable stars in the Galaxy.  相似文献   
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号