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   10190篇
  免费   9284篇
  国内免费   1705篇
航空   17897篇
航天技术   1105篇
综合类   246篇
航天   1931篇
  2024年   63篇
  2023年   221篇
  2022年   349篇
  2021年   442篇
  2020年   517篇
  2019年   1189篇
  2018年   1369篇
  2017年   1317篇
  2016年   1322篇
  2015年   1271篇
  2014年   1099篇
  2013年   1106篇
  2012年   1062篇
  2011年   981篇
  2010年   987篇
  2009年   1008篇
  2008年   887篇
  2007年   729篇
  2006年   575篇
  2005年   404篇
  2004年   381篇
  2003年   316篇
  2002年   351篇
  2001年   291篇
  2000年   263篇
  1999年   282篇
  1998年   233篇
  1997年   205篇
  1996年   157篇
  1995年   135篇
  1994年   139篇
  1993年   193篇
  1992年   136篇
  1991年   313篇
  1990年   262篇
  1989年   294篇
  1988年   207篇
  1987年   82篇
  1986年   32篇
  1983年   4篇
  1981年   3篇
  1972年   1篇
  1962年   1篇
排序方式: 共有10000条查询结果,搜索用时 15 毫秒
21.
河北省农村人口占总人口的79%,是一个比较典型的农业大省。农村生源大学生,是河北省在校大学生的重要组成部分,占生源的最大比例。大学生是宝贵的人才资源,他们的素质尤其是思想政治素质如何,他们能否成为社会主义事业的合格建设者和可靠接班人,是一个非常重要的问题。因而,科学分析和把握他们的思想政治状况,将会增强我们把握大学生思想脉搏的准确性和说服力。为此笔者选取了河北省八个地市的不同高校,进行了问卷调查、座谈和访谈。对河北省农村生源大学生的思想现状进行了调查。通过统计软件的录入和整理,统计结果比较真实地显示了当前河北省农村生源大学生的思想现状。  相似文献   
22.
薄膜充气管充气展开特性试验   总被引:1,自引:0,他引:1  
用展开导轨消除因重力产生的摩擦力,在不同充气速率与初始展开角条件下对薄膜材料充气管的充气展开特性进行了试验研究,获得了展开角,以及展开加速度和内气压的变化规律。试验及分析结果表明:充气管的充气膨胀与展开相互独立,充气膨胀过程近似为等压增容过程,折叠部位的气压变化特性与整体气压变化特性差异明显。  相似文献   
23.
湿度换算软件包   总被引:1,自引:1,他引:0  
湿度不论是在科研领域还是在工业生产中,都是一个很重要的参量指标,在具体的应用中,各领域对湿度参量的使用单位和范围要求是不同的,由此我们编写了一套“湿度换算软件包”,可以在湿度的不同参量和单位间进行换算。本文主要介绍了该软件的主要功能、使用说明以及同国外其它同类软件的数据比对情况。  相似文献   
24.
rom 15 sel     
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   
25.
半实物仿真试验中,要求计算机帧时间与计算积分步长相一致,但在实际试验中不容易精确地做到。本文分析了这种不一致给半实物仿真试验带来的影响,给出了解决的办法,文章中还给出了一实例来说明。  相似文献   
26.
Heavy emission caused by impacting plasma ions results in a fast discharging effect of the initially large surface potentials on the dielectric solar cells. This eventually counteracts the energization process of the plasma ions to the cover glasses and leaves no significant electric fields. Thus, with an existing thermal plasma, electrons are again able to reach dielectric surfaces. Strong localized electric fields of the order of several 10 kV/cm form near the interconnector-cover glass interface.  相似文献   
27.
Using data from the Wide Field Camera EUV all-sky survey, we have established upper limits to the EUV flux from a sample of 30 bright, nearby, non-active spiral galaxies. These galaxies were chosen to be those most likely to be detected in the EUV on the basis of (i) low interstellar absorption within our own galaxy, (ii) brightness in other wavebands, (iii) high star formation activity, and (iv) proximity. The derived EUV upper limits are restrictive, and establish for the first time that the EUV flux escaping from galaxies does not constitute a major component of their bolometric luminosity, and in particular that it cannot be the sink for the energy injected into the interstellar medium by supernova explosions, as had been suggested following the failure to detect this power in the X-ray band.  相似文献   
28.
The authors present a new scientific space mission consisting of a satellite carrying a receiving- only SAR which receives the signal transmitted by the ENVISAT-1 SAR. The integration of ENVISAT-1 SAR and bistatic radar data offers an improved potentiality of surface classification, three-dimensional observation, and the opportunity of advanced scientific experiments in the field of bistatic scattering. The small satellite nominal orbit and the attitude manoeuvres are designed in order to maintain an adequate overlap between the two radar swaths along the whole orbit, taking into account the ENVISAT-1 attitude and pointing. A preliminary satellite design (2-year lifetime) is then performed to evaluate the orbit decay and to determine the appropriate orbit manoeuvres (every 4 days) to control the satellites relative phase. The numerical simulation shows that a spacecraft of about 584kg is able to meet the mission requirements.  相似文献   
29.
In extension to common applications such as groundtrack displays and antenna steering, the SGP4 orbit model is proposed for operational orbit determination in small satellite missions. SGP4 is an analytical orbit model for Low-Earth orbiting satellites that is widely used for the propagation of NORAD twoline elements. Twoline elements may hence be generated completely independent of NORAD. Their use as exclusive source of orbital information simplifies the operations concept and reduces mission costs through the extensive use of existing low-cost mission support software. Due to small computer resource requirements of 8–10kByte, the SGP4 model may also be applied for onboard orbit computations making use of e.g. a 80186 processor, thus ensuring full compatibility of ground-based and onboard operations. The proposed approach is particularly suited in combination with a space-borne GPS receiver, were the C/A-code navigation solutions are treated as measurements that are adjusted in a least-squares sense using the SGP4 model. As consequence, inherent drawbacks of the pure navigation solutions such as data gaps and scatter as well as limited velocity accuracy are avoided, while the operational navigation activities are kept at a minimum. The feasibility of the concept is illustrated based on real GPS navigation data from the TOPEX/Poseidon and the MIR space station with an inherent data quality of 50–100 m. It is shown that 3 hours of data within a 4 day period are sufficient to keep the position error within 4 km, that is considered sufficient for most applications.  相似文献   
30.
赵坚行  易勇 《推进技术》1993,14(3):8-15
本文对k-ε-g紊流燃烧模型中模型系数C_R,C_(g1),C_(g2)的选定和计算浓度脉动均方值g的不同方法进行数值研究。计算结果表明模型系数值的选定直接与化学反应速率有关,而其中C_R影响最大。g的计算虽然可有不同方法,而其中微分方程求解最佳。并用实验数据来验证计算结果。  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