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   3072篇
  免费   21篇
  国内免费   9篇
航空   1174篇
航天技术   1159篇
综合类   22篇
航天   747篇
  2022年   11篇
  2021年   34篇
  2019年   14篇
  2018年   78篇
  2017年   61篇
  2016年   62篇
  2015年   24篇
  2014年   87篇
  2013年   88篇
  2012年   90篇
  2011年   143篇
  2010年   105篇
  2009年   168篇
  2008年   224篇
  2007年   98篇
  2006年   76篇
  2005年   105篇
  2004年   105篇
  2003年   109篇
  2002年   77篇
  2001年   131篇
  2000年   52篇
  1999年   73篇
  1998年   76篇
  1997年   44篇
  1996年   76篇
  1995年   60篇
  1994年   63篇
  1993年   38篇
  1992年   57篇
  1991年   19篇
  1990年   25篇
  1989年   57篇
  1988年   24篇
  1987年   24篇
  1986年   30篇
  1985年   84篇
  1984年   59篇
  1983年   47篇
  1982年   55篇
  1981年   89篇
  1980年   21篇
  1979年   13篇
  1978年   12篇
  1977年   18篇
  1976年   12篇
  1975年   16篇
  1974年   18篇
  1973年   10篇
  1970年   7篇
排序方式: 共有3102条查询结果,搜索用时 15 毫秒
991.
Performance prediction in preliminary design stages of several turbomachinery components is a critical task in order to bring the design processes of these devices to a successful conclusion.In this paper,a review and analysis of the major loss mechanisms and loss models,used to determine the efficiency of a single stage centrifugal compressor,and a subsequent examination to determine an appropriate loss correlation set for estimating the isentropic efficiency in preliminary design stages of centrifugal compressors,were developed.Several semi-empirical correlations,commonly used to predict the efficiency of centrifugal compressors,were implemented in FORTRAN code and then were compared with experimental results in order to establish a loss correlation set to determine,with good approximation,the isentropic efficiency of single stage compressor.The aim of this study is to provide a suitable loss correlation set for determining the isentropic efficiency of a single stage centrifugal compressor,because,with a large amount of loss mechanisms and correlations available in the literature,it is difficult to ascertain how many and which correlations to employ for the correct prediction of the efficiency in the preliminary stage design of a centrifugal compressor.As a result of this study,a set of correlations composed by nine loss mechanisms for single stage centrifugal compressors,conformed by a rotor and a diffuser,are specified.  相似文献   
992.
Cosmic Research - A special version of the SHIELD transport code has been developed intended for radiation protection purposes in space. The calculation of the fluxes of primary and secondary...  相似文献   
993.
Gaillard  F.  Bouhifd  M. A.  Füri  E.  Malavergne  V.  Marrocchi  Y.  Noack  L.  Ortenzi  G.  Roskosz  M.  Vulpius  S. 《Space Science Reviews》2021,217(1):1-28
Space Science Reviews - Accretion onto black holes is an efficient mechanism in converting the gas mass-energy into energetic outputs as radiation, wind and jet. Tidal disruption events, in which...  相似文献   
994.
Frolov  V. L.  Luk’yanova  R. Yu.  Ryabov  A. O.  Bolotin  I. A. 《Cosmic Research》2021,59(4):231-249
Cosmic Research - We have analyzed the experimental data obtained in 2016–2019 from the measurements of plasma disturbances and electric currents induced at ionospheric altitudes upon the...  相似文献   
995.
996.
A technique that allows simultaneous heating of the heat-exchange surface and estimation of its local temperature from the corresponding electrical resistance of the heating element is presented. The systematic error in measurements of the local heat transfer coefficient has been analyzed. A relation that takes possible heat loss into account and minimizes the measurement errors has been obtained.  相似文献   
997.
The Rosetta Orbiter Spectrometer for Ion and Neutral Analysis (ROSINA) instrument onboard the Rosetta spacecraft has measured molecular oxygen (O2) in the coma of comet 67P/Churyumov-Gerasimenko (67P/C-G) in surprisingly high abundances. These measurements mark the first unequivocal detection of O2 in a cometary environment. The large relative abundance of O2 in 67P/C-G despite its high reactivity and low interstellar abundance poses a puzzle for its origin in comet 67P/C-G, and potentially other comets. Since its detection, there have been a number of hypotheses put forward to explain the production and origin of O2 in the comet. These hypotheses cover a wide range of possibilities from various in situ production mechanisms to protosolar nebula and primordial origins. Here, we review the O2 formation mechanisms from the literature, and provide a comprehensive summary of the current state of knowledge of the sources and origin of cometary O2.  相似文献   
998.
The algorithms for achieving a practical increase in the rate of data transmission on the space-craft–ground tracking station line has been considered. This increase is achieved by applying spectral-effective modulation techniques, the technology of orthogonal frequency compression of signals using millimeterrange radio waves. The advantages and disadvantages of each of three algorithms have been revealed. A significant advantage of data transmission in the millimeter range has been indicated.  相似文献   
999.
Superluminous supernovae are a new class of supernovae that were recognized about a decade ago. Both observational and theoretical progress has been significant in the last decade. In this review, we first briefly summarize the observational properties of superluminous supernovae. We then introduce the three major suggested luminosity sources to explain the huge luminosities of superluminous supernovae, i.e., the nuclear decay of 56Ni, the interaction between supernova ejecta and dense circumstellar media, and the spin down of magnetars. We compare these models and discuss their strengths and weaknesses.  相似文献   
1000.
In the design of an aircraft at the stage of selecting its geometrical parameters, a method is proposed for evaluating the performance capabilities of manual control to ensure the quality of a given flight stabilization mode. The attainability of the given aircraft-pilot dynamic properties is evaluated by a frequency-domain method for permissible values of the aircraft and the pilot model parameters. The quality of the manual control for the longitudinal motion of the aircraft is evaluated.  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