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   4009篇
  免费   4篇
  国内免费   21篇
航空   2083篇
航天技术   1108篇
综合类   10篇
航天   833篇
  2019年   19篇
  2018年   194篇
  2017年   157篇
  2016年   53篇
  2015年   36篇
  2014年   56篇
  2013年   78篇
  2012年   104篇
  2011年   244篇
  2010年   200篇
  2009年   249篇
  2008年   268篇
  2007年   213篇
  2006年   76篇
  2005年   135篇
  2004年   102篇
  2003年   90篇
  2002年   57篇
  2001年   84篇
  2000年   50篇
  1999年   66篇
  1998年   82篇
  1997年   52篇
  1996年   63篇
  1995年   79篇
  1994年   77篇
  1993年   53篇
  1992年   64篇
  1991年   34篇
  1990年   30篇
  1989年   72篇
  1988年   29篇
  1987年   31篇
  1986年   35篇
  1985年   124篇
  1984年   68篇
  1983年   59篇
  1982年   58篇
  1981年   105篇
  1980年   36篇
  1979年   27篇
  1978年   25篇
  1977年   28篇
  1976年   18篇
  1975年   32篇
  1974年   19篇
  1973年   27篇
  1972年   20篇
  1970年   24篇
  1969年   26篇
排序方式: 共有4034条查询结果,搜索用时 15 毫秒
951.
This paper proposes to solve the problem of determining the strength properties of materials for thin-walled structural elements under mechanical and thermal loading as an optimization problem. A mathematical statement of the problem under certain assumptions is given.  相似文献   
952.
A computational technique, developed for analysis of strength, stability and low-cycle durability of GTE exhaust frame complex structure under operational and emergency loads is described. The presented technique, based on the ANSYS and STAR-CD engineering analysis software, and self-design software can improve the accuracy and efficiency of calculations, and reduce efforts on finite element mesh development, performing calculations and processing of results.  相似文献   
953.
The stress-strain state of thin-walled aircraft structures such as a wing or fuselage made of composite materials is determined based on the beam theory. The laminated skin is orthotropic. The solution was obtained without using the centroidal principal section axes and subdividing the problem in shear and torsion. A calculation variant with skin discretization along the section contour was studied.  相似文献   
954.
Based on the experimental data, a dependence of the minimal friction losses in cascades was obtained. A turbine stage efficiency gain as a result of cascade improvement over the last three decades of the 20th century was estimated by this dependence.  相似文献   
955.
Space plasmas are host to the electrostatic Langmuir waves and a rich range of processes associated with them. Many of such processes that are of interest in micro-scale plasma physics and magnetosphere-ionosphere physics are open to investigation via incoherent scatter plasma lines—i.e., a pair of resonant peaks in the incoherent scatter radar (ISR) spectrum, symmetrically displaced from the radar transmitting frequency by about the plasma frequency, as the signature of Langmuir waves in the ISR spectrum. There now exists a large body of literature devoted to the investigation of a number of topics in ionospheric physics via plasma line theory and observation. It is the goal of this work to provide a comprehensive review of this literature, from the early theoretical works on oscillations in magnetized plasma to the recent advances in plasma line measurements and applications. This review includes detailed theoretical discussions on the intensity and frequency displacement of plasma lines. It reviews the experimental observations of plasma lines enhanced by various sources of energy and discusses the implications of the observations in the context of ionospheric physics. The review also covers the practical aspects of plasma line measurements, from measurement techniques to the applications of plasma lines in estimating the bulk parameters of the ionosphere.  相似文献   
956.
A technique is suggested for calculating the helicopter spatial motion and the stress-strain state of a skid landing gear in the course of landing with regard for the second landing impact; geometric, material and design nonlinearity of undercarriage springs deformation is taken into account. The comparison between the analysis results and experimental data is presented.  相似文献   
957.
958.
959.
The new conceptual design of simple gas turbine engines for different purposes is presented. A choked-flow low-pressure turbine is used that allows reducing the number of stages and gas temperature in the relative motion ahead of blades. Application of such turbines with uncooled blades to reduce the cost of power-limited engines is considered.  相似文献   
960.
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