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   748297篇
  免费   8435篇
  国内免费   2199篇
电工技术   13594篇
综合类   956篇
化学工业   115669篇
金属工艺   30138篇
机械仪表   23449篇
建筑科学   17138篇
矿业工程   5085篇
能源动力   19390篇
轻工业   60450篇
水利工程   8848篇
石油天然气   17929篇
武器工业   76篇
无线电   81830篇
一般工业技术   151530篇
冶金工业   131797篇
原子能技术   18519篇
自动化技术   62533篇
  2021年   6779篇
  2019年   6442篇
  2018年   11135篇
  2017年   11366篇
  2016年   11905篇
  2015年   7571篇
  2014年   12801篇
  2013年   34121篇
  2012年   19963篇
  2011年   27154篇
  2010年   21676篇
  2009年   24382篇
  2008年   24752篇
  2007年   24473篇
  2006年   21173篇
  2005年   19376篇
  2004年   18800篇
  2003年   18329篇
  2002年   17714篇
  2001年   17297篇
  2000年   16474篇
  1999年   16636篇
  1998年   39155篇
  1997年   28305篇
  1996年   21918篇
  1995年   16888篇
  1994年   15118篇
  1993年   14935篇
  1992年   11345篇
  1991年   11003篇
  1990年   10736篇
  1989年   10486篇
  1988年   9981篇
  1987年   9038篇
  1986年   8861篇
  1985年   9934篇
  1984年   9061篇
  1983年   8582篇
  1982年   7799篇
  1981年   7913篇
  1980年   7645篇
  1979年   7576篇
  1978年   7526篇
  1977年   8293篇
  1976年   10544篇
  1975年   6661篇
  1974年   6400篇
  1973年   6474篇
  1972年   5520篇
  1971年   5072篇
排序方式: 共有10000条查询结果,搜索用时 15 毫秒
1.
2.
3.
4.
5.
6.
7.
The results of a system analysis of the efficiency of nitrous oxide(N_2O) as a propellant component for small space vehicles(SSV) were presented. A criterion for mass efficiency of the SSV propulsion system(PS) is determined. The current global state-of-the-art of SSV PSs is shown. The application field of nitrous oxide in SSV PSs is calculated and mass efficiency of N_2O application is quantitatively determined. An overview of physical and chemical as well as operational properties of nitrous oxide as a promising, non-toxic component of rocket propellant is provided. Main physical and chemical constants of gaseous and liquid nitrous oxide; chemical properties of N_2O, thermal stability of N_2O, catalytic decomposition of N_2O, a mechanism of decomposition of N_2O, catalysts for decomposition of N_2O, ballast additives to N_2O, application of nitrous oxide, nitrous oxide as a rocket propellant, production of nitrous oxide, toxicity of nitrous oxide, fire hazard of N_2O, requirements to equipment when handling N_2O; storage and transportation of N_2O are considered. It is demonstrated that nitrous oxide is a chemical compound meeting the requirements to rocket propellants, including those related to the environmental friendliness of propellants. With 75 references.  相似文献   
8.
9.
Temperature history can have a significant effect on the strength of water-saturated chalk.In this study,hydrostatic stress cycles are applied to understand the mechanical response of chalk samples exposed to temperature cycling between each stress cycle,compared to the samples tested at a constant temperature.The total accumulated strain during a stress cycle and the irreversible strain are reported.Chalk samples from Kansas(USA)and Mons(Belgium),with different degrees of induration(i.e.amount of contact cementation),were used.The samples were saturated with equilibrated water(polar)and nonpolar Isopar H oil to quantify water weakening.All samples tested during 10 stress cycles with varying temperature(i.e.temperature cycled in between each stress cycle)accumulated more strain than those tested at constant temperatures.All the stress cycles were performed at 30℃.The two chalk types behaved similarly when saturated with Isopar H oil,but differently when saturated with water.When saturated with water,the stronger Kansas chalk accumulated more total strain and more irreversible strain within each stress cycle than the weaker Mons chalk.  相似文献   
10.
This paper introduces two novel nonlinear stochastic attitude estimators developed on the Special Orthogonal Group with the tracking error of the normalized Euclidean distance meeting predefined transient and steady‐state characteristics. The tracking error is confined to initially start within a predetermined large set such that the transient performance is guaranteed to obey dynamically reducing boundaries and decrease smoothly and asymptotically to the origin in probability from almost any initial condition. The proposed estimators produce accurate attitude estimates with remarkable convergence properties using measurements obtained from low‐cost inertial measurement units. The estimators proposed in continuous form are complemented by their discrete versions for the implementation purposes. The simulation results illustrate the effectiveness and robustness of the proposed estimators against uncertain measurements and large initialization error, whether in continuous or discrete form.  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