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   5797篇
  免费   474篇
  国内免费   593篇
化学   742篇
晶体学   14篇
力学   721篇
综合类   87篇
数学   4119篇
物理学   1181篇
  2024年   3篇
  2023年   74篇
  2022年   134篇
  2021年   127篇
  2020年   190篇
  2019年   176篇
  2018年   160篇
  2017年   190篇
  2016年   181篇
  2015年   133篇
  2014年   225篇
  2013年   442篇
  2012年   278篇
  2011年   356篇
  2010年   304篇
  2009年   461篇
  2008年   423篇
  2007年   399篇
  2006年   356篇
  2005年   328篇
  2004年   239篇
  2003年   234篇
  2002年   203篇
  2001年   162篇
  2000年   155篇
  1999年   136篇
  1998年   166篇
  1997年   114篇
  1996年   96篇
  1995年   53篇
  1994年   52篇
  1993年   39篇
  1992年   43篇
  1991年   32篇
  1990年   22篇
  1989年   20篇
  1988年   22篇
  1987年   19篇
  1986年   18篇
  1985年   12篇
  1984年   18篇
  1983年   5篇
  1982年   10篇
  1981年   10篇
  1980年   9篇
  1979年   9篇
  1978年   10篇
  1975年   2篇
  1974年   3篇
  1972年   3篇
排序方式: 共有6864条查询结果,搜索用时 15 毫秒
91.
Correlation of swirl number for a radial-type swirl generator   总被引:1,自引:0,他引:1  
An experimental investigation was undertaken to derive a new correlation for the swirl number of a radial-type swirl generator under various Reynolds numbers and various vane angle conditions. A radial-type swirl generator with 16 rotary guide vanes was used to generate an annular swirling jet flow. The Reynolds numbers ranged from 60 to 6000, and the vane angles from 0° to 56°. Quantitative measurements for the velocities were made by using an optical method of laser-Doppler anemometry (LDA). Three-component velocity profiles of axial, radial, and azimuthal components at the swirling jet exit were measured for various flow conditions. A flow visualization method using smoke-wire and still photography was also applied to observe the flow patterns of the recirculation region behind the circular bluff body. Under low Reynolds number conditions, the swirl strength was found to be strongly dependent on the Reynolds number as well as on the guide vane angle. Based on the experimental results, a modified swirl number S is derived to characterize the swirling flow, which is useful for the design of a swirl generator.  相似文献   
92.
圆柱尾流的绝对不稳定性   总被引:3,自引:0,他引:3  
在水槽和低湍流度水洞中进行亚临界雷诺数圆柱尾流稳定性实验来流速度由零缓慢增长到一定值后保持不变,稳定足够长时间后,在流向某站位处给流场一个有限幅值的脉冲扰动,测量扰动前后相当长时间内下游尾流速度信号的变化情况当雷诺数处于高亚临界值时,未受扰动的尾流速度脉动很小,处于定常状态,但对近尾流进行脉冲扰动后,能够激发出不衰减的旋涡脱落发现扰动位置限制在圆柱后一定范围内才能有效,再往下游则扰动随时间衰减.说明圆柱近尾流中存在一个绝对不稳定区,在该区域内的扰动将在当地放大,经过复杂的演化,最后形成不衰减的旋涡脱落.  相似文献   
93.
In this study, we have investigated the influence of shape of planar contractions on the orientation distribution of stiff fibers suspended in turbulent flow. To do this, we have employed a model for the orientational diffusion coefficient based on the data obtained by high-speed imaging of suspension flow at the centerline of a contraction with flat walls. This orientational diffusion coefficient depends only on the contraction ratio and turbulence intensity. Our measurements show that the turbulence intensity decays exponentially independent of the contraction angle. This implies that the turbulence variation in the contraction is independent of the shape, consistent with the results by the rapid distortion theory and the experimental results of axisymmetric contractions. In order to determine the orientation anisotropy, we have solved a Fokker–Planck type equation governing the orientation distribution of fibers in turbulent flow. Although the turbulence variation and the orientational diffusion are independent of the contraction shape, the results show that the variation of the orientation anisotropy is dependent on shape. This can be explained by the variation of the rotational Péclet number, Per, inside the contractions. This quantity is a measure of the importance of the mean rate of the strain relative to the orientational diffusion. We have shown that when Per < 10 turbulence can significantly influence the evolution of the orientation anisotropy. Since in contractions with identical inlet conditions the streamwise position where Per = 10 depends on the shape, the orientation anisotropy is dependent on the variation of rate of strain in a given contraction. We demonstrate the shape effect by considering contraction with flat walls as well as three contractions with different mean rate of strain variation.  相似文献   
94.
等速上仰翼型动态失速现象研究   总被引:9,自引:0,他引:9  
白鹏  崔尔杰  周伟江  李锋 《力学学报》2004,36(5):569-576
翼型大迎角绕流的静态失速将造成升力突降和气动性能急剧恶化,但利用非定常运动所产生 的动态失速效应,可以大大地延缓气流分离和失速现象的发生. 采用Rogers发 展的双时间步Roe格式,求解拟压缩性修正不可压N-S方程. 数值模拟了低雷诺数 ($Re=4.8 \times 10^{4}$)条件下NACA0015翼型作等速上仰($\alpha =0^{\circ} \sim 60^{\circ}$)的动态失速过程,同Walker的试验结果比 较,验证了计算结果的正确性. 研究了该过程中主涡、二次涡和三次涡的发展,升 力系数随攻角变化,以及不同上仰速度对动态失速效应所造成的影响.  相似文献   
95.
腐蚀磨损协同作用率的研究   总被引:7,自引:5,他引:7  
提出了腐蚀与磨损“协同作用”的概念,并用于判断腐蚀与磨损协同作用的性质及大小和确定腐蚀磨损过程中材料损失的主要形式。介绍了协同作用率的测定方法,并以G105钢及化学镀Ni-P合金在5.0%NaCl溶液中的腐蚀腐损作为研究对象,研究了载荷、滑动速度对腐蚀磨损协同作用的影响。结果表明:协同作用率随载荷增大而增大,随滑动速度增大而减小。  相似文献   
96.
稳恒扩展裂纹尖端的弹粘塑性场   总被引:16,自引:0,他引:16  
采用弹粘塑性力学模型代替通常的弹塑性模型,对于I型和Ⅱ型问题,分别求得了不可压缩材料中平面应变动态扩展裂纹尖端的指数奇异性场和对数奇异性场,消除了弹塑性解中存在的塑性激波。通过数值计算,分别求得了两种奇异属性的分界线,建立起统一的裂纹尖端奇异性场。  相似文献   
97.
Magyari  E.  Keller  B. 《Transport in Porous Media》2003,51(2):227-230
External free convection boundary-layer flows are usually treated by neglecting the effect of viscous dissipation. This assumption always results in a non-parallel flow, besides a strong parallel component also a weak transversal component of the (steady) velocity field occurs. The present paper shows, however, that the weak opposing effect of the buoyancy forces due to heat release by viscous dissipation, can give rise along a cold vertical plate adjacent to a fluid saturated porous medium to a strictly parallel steady free convection flow. This boundary-layer flow is described by an algebraically decaying exact analytical solution of the basic balance equations.  相似文献   
98.
柏楠  邓学蓥  王延奎 《力学学报》2007,39(2):261-266
通过在细长旋成体模型机身的不同位置设置出烟孔,使用新型发烟装置对模型注入雾化油 滴,采用激光片光法在常规风洞中高风速(60m/s)条件下得到清晰、完整而稳定的截面涡 结构图像. 并通过同状态标定法和等比例网格法发展了简易涡位定量测量技术,为前体非对 称涡Re数效应的研究提供了重要的技术平台.  相似文献   
99.
An analysis is presented for the problem of free convection with mass transfer flow for a micropolar fluid via a porous medium bounded by a semi-infinite vertical porous plate in the presence of a transverse magnetic field. The plate moves with constant velocity in the longitudinal direction, and the free stream velocity follows an exponentially small perturbation law. A uniform magnetic field acts perpendicularly to the porous surface in which absorbs the micropolar fluid with a suction velocity varying with time. Numerical results of velocity distribution of micropolar fluids are compared with the corresponding flow problems for a Newtonian fluid. Also, the results of the skin-friction coefficient, the couple stress coefficient, the rate of the heat and mass transfers at the wall are prepared with various values of fluid properties and flow conditions.  相似文献   
100.
RESISTANCE EFFECT OF ELECTRIC DOUBLE LAYER ON LIQUID FLOW IN MICROCHANNEL   总被引:1,自引:0,他引:1  
Poisson-Boltzrnann equation for EDL (electric double layer) and Navier-Stokes equation for liquid flows were numerically solved to investigate resistance effect of electric double layer on liquid flow in microchannel. The dimension analysis indicates that the resistance effect of electric double layer can be estimated by an electric resistance number, which is proportional to the square of the liquid dielectric constant and the solid surface zeta potential, and inverse-proportional to the liquid dynamic viscosity, electric conductivity and the square of the channel width. An "electric current density balancing" (ECDB) condition was proposed to evaluate the flow-induced streaming potential, instead of conventional "electric current balancing" (ECB) condition which may induce spurious local backflow in neighborhood of the solid wall of the microchannel. The numerical results of the flow rate loss ratio and velocity profile are also given to demonstrate the resistance effect of electric double layer in microchannel.  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