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   3872篇
  免费   44篇
  国内免费   29篇
航空   1866篇
航天技术   1357篇
综合类   71篇
航天   651篇
  2021年   38篇
  2018年   62篇
  2017年   67篇
  2016年   37篇
  2015年   38篇
  2014年   76篇
  2013年   108篇
  2012年   90篇
  2011年   169篇
  2010年   115篇
  2009年   149篇
  2008年   212篇
  2007年   124篇
  2006年   122篇
  2005年   123篇
  2004年   83篇
  2003年   119篇
  2002年   92篇
  2001年   109篇
  2000年   93篇
  1999年   103篇
  1998年   109篇
  1997年   103篇
  1996年   93篇
  1995年   108篇
  1994年   109篇
  1993年   64篇
  1992年   76篇
  1991年   42篇
  1990年   45篇
  1989年   77篇
  1988年   39篇
  1987年   32篇
  1986年   35篇
  1985年   115篇
  1984年   87篇
  1983年   85篇
  1982年   67篇
  1981年   111篇
  1980年   26篇
  1979年   27篇
  1978年   34篇
  1977年   25篇
  1976年   24篇
  1975年   40篇
  1974年   20篇
  1972年   33篇
  1971年   25篇
  1969年   23篇
  1967年   24篇
排序方式: 共有3945条查询结果,搜索用时 578 毫秒
811.
麻花钻钻尖锥面刃磨参数优化求解   总被引:1,自引:0,他引:1  
麻花钻锥面刃磨方法有4个刃磨参数,当给定外缘转点的结构圆周后角、横刃斜角、锋角这3个结构参数时,后刀面的形状并不唯一.为了获得唯一的后刀面廓形,必须增加一个辅助参数.可供选择的补充参数有尾隙角、横刃后角、周边后角、切深后角等.这样,当给定一个补充参数后,4个设计参数就可以决定4个刃磨参数.然而单独使用某一个补充参数,就忽略了其余参数的影响.采用优化的方法来求解刃磨参数,将各个补充参数和刃磨参数的实际可调范围作为约束条件,就可以得到满足一定要求的最优解.  相似文献   
812.
箔条云团的布朗运动扩散模型   总被引:9,自引:0,他引:9  
假定箔条所在位置处大气运动速度是一个维纳随机过程,同时在忽略箔条的质量时箔条的运动完全反应当地大气的运动,在此基础上建立箔条云团的扩散模型及数值仿真模型. 对扩散模型进行分析得到了箔条云团扩散过程中的数字特征.对数值仿真模型的分析表明必须对大气的运动方差进行时间离散化补偿,进行离散化补偿后箔条云团的数字特征不受模拟时时间步长的影响.模拟结果证明了分析的正确性.  相似文献   
813.
 共形微带天线间的互耦对微带天线阵的性能有重要影响,另一方面,为了防止对微带天线阵的自然的或人为的损害,需要在天线阵表面涂覆介质层或给其加上天线罩,因此在设计共形微带天线与阵列时也应当考虑覆盖层或天线罩的影响.利用严格的全波法分析和计算了介质覆盖、探针馈电的柱面共形微带天线单元间的互耦,给出了E面和H面互耦的数值结果,并讨论了柱面曲率半径和贴片间距对互耦的影响,给出了互耦随频率的变化关系,同时也研究了衬底介质和覆盖层对互耦的作用.  相似文献   
814.
有限平面上圆口径辐射场的数值分析   总被引:1,自引:1,他引:0  
计算由TE11模激励的圆波导末端开口所形成的圆口径天线的辐射场.首先利用等效原理和矩量法计算嵌在无限大金属板上圆口径的等效磁流分布,允许圆波导中有任意多个高次模式存在,利用傅里叶变换法求得其辐射方向图,然后把该辐射场作为有限接地板边缘的入射场,利用几何绕射理论(GTD)计算有限接地板对圆口径方向图的贡献,其中在焦散区及接近焦散区区域采用等效磁流法计算有限接地板的影响,给出计算公式及计算例子,部分结果得到了文献的验证.  相似文献   
815.
Space-time adaptive processing (STAP) and related adaptive array techniques hold tremendous potential for improving sensor performance by exploiting signal diversity. Such methods have important application in radar, sonar, and communication systems. Recent advances in digital signal processing technology now provide the computational means to field STAP-based systems. The objective of this special collection of papers is to examine the current state-of-the art in STAP technology and explore the remaining obstacles, practical issues and novel techniques required to implement STAP-based radar, sonar or communication systems  相似文献   
816.
Green  J.L.  Benson  R.F.  Fung  S.F.  Taylor  W.W.L.  Boardsen  S.A.  Reinisch  B.W.  Haines  D.M.  Bibl  K.  Cheney  G.  Galkin  I.A.  Huang  X.  Myers  S.H.  Sales  G.S.  Bougeret  J.-L.  Manning  R.  Meyer-Vernet  N.  Moncuquet  M.  Carpenter  D.L.  Gallagher  D.L.  Reiff  P.H. 《Space Science Reviews》2000,91(1-2):361-389
The Radio Plasma Imager (RPI) will be the first-of-its kind instrument designed to use radio wave sounding techniques to perform repetitive remote sensing measurements of electron number density (N e) structures and the dynamics of the magnetosphere and plasmasphere. RPI will fly on the Imager for Magnetopause-to-Aurora Global Exploration (IMAGE) mission to be launched early in the year 2000. The design of the RPI is based on recent advances in radio transmitter and receiver design and modern digital processing techniques perfected for ground-based ionospheric sounding over the last two decades. Free-space electromagnetic waves transmitted by the RPI located in the low-density magnetospheric cavity will be reflected at distant plasma cutoffs. The location and characteristics of the plasma at those remote reflection points can then be derived from measurements of the echo amplitude, phase, delay time, frequency, polarization, Doppler shift, and echo direction. The 500 m tip-to-tip X and Y (spin plane) antennas and 20 m Z axis antenna on RPI will be used to measures echoes coming from distances of several R E. RPI will operate at frequencies between 3 kHz to 3 MHz and will provide quantitative N e values from 10–1 to 105 cm–3. Ray tracing calculations, combined with specific radio imager instrument characteristics, enables simulations of RPI measurements. These simulations have been performed throughout an IMAGE orbit and under different model magnetospheric conditions. They dramatically show that radio sounding can be used quite successfully to measure a wealth of magnetospheric phenomena such as magnetopause boundary motions and plasmapause dynamics. The radio imaging technique will provide a truly exciting opportunity to study global magnetospheric dynamics in a way that was never before possible.  相似文献   
817.
本文使用了两种类型等参元,通过变分法,计算了三维机翼亚临界定常位势流中的压力分布,计算结果与试验结果符合较好。文中还使用了有限元法中的局部线性化理论,插值出元素中心点密度去处理迭代过程中元素系数阵的计算,其结果与通常的有限元计算相吻合,但计算时间却明显减少了。文中还对有限元法局部线性化理论和局部线性化有限元法做了阐述。  相似文献   
818.
The Radio Plasma Imager investigation on the IMAGE spacecraft   总被引:1,自引:0,他引:1  
Reinisch  B.W.  Haines  D.M.  Bibl  K.  Cheney  G.  Galkin  I.A.  Huang  X.  Myers  S.H.  Sales  G.S.  Benson  R.F.  Fung  S.F.  Green  J.L.  Boardsen  S.  Taylor  W.W.L.  Bougeret  J.-L.  Manning  R.  Meyer-Vernet  N.  Moncuquet  M.  Carpenter  D.L.  Gallagher  D.L.  Reiff  P. 《Space Science Reviews》2000,91(1-2):319-359
Radio plasma imaging uses total reflection of electromagnetic waves from plasmas whose plasma frequencies equal the radio sounding frequency and whose electron density gradients are parallel to the wave normals. The Radio Plasma Imager (RPI) has two orthogonal 500-m long dipole antennas in the spin plane for near omni-directional transmission. The third antenna is a 20-m dipole along the spin axis. Echoes from the magnetopause, plasmasphere and cusp will be received with the three orthogonal antennas, allowing the determination of their angle-of-arrival. Thus it will be possible to create image fragments of the reflecting density structures. The instrument can execute a large variety of programmable measuring options at frequencies between 3 kHz and 3 MHz. Tuning of the transmit antennas provides optimum power transfer from the 10 W transmitter to the antennas. The instrument can operate in three active sounding modes: (1) remote sounding to probe magnetospheric boundaries, (2) local (relaxation) sounding to probe the local plasma frequency and scalar magnetic field, and (3) whistler stimulation sounding. In addition, there is a passive mode to record natural emissions, and to determine the local electron density, the scalar magnetic field, and temperature by using a thermal noise spectroscopy technique.  相似文献   
819.
Duldig  Marc L. 《Space Science Reviews》2000,93(1-2):207-226
Muon observations are complementary to neutron monitor observations but there are some important differences in the two techniques. Unlike neutron monitors, muon telescope systems use coincidence techniques to obtain directional information about the arriving particle. Neutron monitor observations require simple corrections for pressure variations to compensate for the varying mass of atmospheric absorber over a site. In contrast, muon observations require additional corrections for the positive and negative temperature effects. Muon observations commenced many years before neutron monitors were constructed. Thus, muon data over a larger number of solar cycles is available to study solar modulation on anisotropies and other cosmic ray variations. The solar diurnal and semi-diurnal variations have been studied for many years. Using the techniques of Bieber and Chen it has been possible to derive the radial gradient, parallel mean-free path and symmetric latitude gradient of cosmic rays for rigidities <200 GV. The radial gradient varies with the 11-year solar activity cycle whereas the parallel mean-free path appears to vary with the 22-year solar magnetic cycle. The symmetric latitudinal gradient reverses at each solar polarity reversal. These results are in general agreement with predictions from modulation models. In undertaking these analyses the ratio of the parallel to perpendicular mean-free path must be assumed. There is strong contention in the literature about the correct value to employ but the results are sufficiently robust for this to be, at most, a minor problem. An asymmetric latitude gradient of highly variable nature has been found. These observations do not support current modulation models. Our view of the sidereal variation has undergone a revolution in recent times. Nagashima, Fujimoto and Jacklyn proposed a narrow Tail-In source anisotropy and separate Loss-Cone anisotropy as being responsible for the observed variations. A new analysis technique, more amenable to such structures, was developed by Japanese and Australian researchers. They confirmed the existence of the two anisotropies. However, they found that the Tail-In anisotropy is asymmetric and that both anisotropies had different positions from the prediction. Most 27-day modulations are observed at neutron monitor rigidities but not so readily at higher rigidities. An exception to this is the Isotropic Intensity Wave modulation observed in the early 1980s and again in 1991. This modulation is very strongly related to the heliospheric sector structure and implies a significantly different cosmic ray density on either side of the neutral sheet. The interpretation of most cosmic ray modulation phenomena requires good latitude coverage in both hemispheres. The closure of many muon observatories is a matter of concern. In the northern hemisphere a few new instruments are being constructed and spatial coverage is barely adequate. In the southern hemisphere the situation is far worse with the possibility that within a decade only the Mawson observatory in Antarctica will still be in operation. This revised version was published online in August 2006 with corrections to the Cover Date.  相似文献   
820.
空间级加成型室温硫化硅橡胶粘结剂的研究   总被引:4,自引:1,他引:3       下载免费PDF全文
研究了一种新的空间级加成型室温硫化硅橡胶KH—SP—B ,它的特点在于具有低的热真空失重 ,在 12 5℃× 2 4h ,1× 10 - 10 MPa下的热真空失重可小于 0 .3% ;高的粘接强度 ,与金属及聚酰亚胺等的粘结强度可达到 2MPa以上 ;高的热稳定性能 ,分解温度可达 52 4℃ ;优异的低温性能 ,脆性温度为 - 114℃ ;良好的电性能 ,体积电阻率可达 1.3× 10 16 Ω·cm。是一种综合性能优良的空间级室温硫化硅橡胶。  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