全文获取类型
收费全文 | 1914篇 |
免费 | 382篇 |
国内免费 | 517篇 |
专业分类
航空 | 1797篇 |
航天技术 | 330篇 |
综合类 | 340篇 |
航天 | 346篇 |
出版年
2024年 | 7篇 |
2023年 | 30篇 |
2022年 | 58篇 |
2021年 | 85篇 |
2020年 | 92篇 |
2019年 | 89篇 |
2018年 | 99篇 |
2017年 | 110篇 |
2016年 | 118篇 |
2015年 | 106篇 |
2014年 | 143篇 |
2013年 | 112篇 |
2012年 | 159篇 |
2011年 | 142篇 |
2010年 | 141篇 |
2009年 | 132篇 |
2008年 | 111篇 |
2007年 | 131篇 |
2006年 | 115篇 |
2005年 | 90篇 |
2004年 | 76篇 |
2003年 | 55篇 |
2002年 | 63篇 |
2001年 | 55篇 |
2000年 | 42篇 |
1999年 | 42篇 |
1998年 | 45篇 |
1997年 | 42篇 |
1996年 | 57篇 |
1995年 | 41篇 |
1994年 | 53篇 |
1993年 | 36篇 |
1992年 | 30篇 |
1991年 | 37篇 |
1990年 | 20篇 |
1989年 | 29篇 |
1988年 | 14篇 |
1987年 | 2篇 |
1986年 | 4篇 |
排序方式: 共有2813条查询结果,搜索用时 718 毫秒
581.
582.
583.
对将增强碳/碳纤维块体切削成球锥外形的工艺,块体热膨胀系数异性轴指向可以极大地影响球锥热应力大小,存在优化设计的潜力。本文对增强碳/碳不同主轴方向弹性模量比值下的球锥最小热应力优化特性进行了研究,发现以1为界,不同模量对比关系下的优化特征是完全不同的。在本文加热条件下,当异性轴模量小于同性面模量时,优化曲线对温度场变化很敏感,以块体异性轴和球锥横截面成±42.9夹角时热应力最小;当异性轴模量大于同性面模量时,优化曲线随加热时间变化不大,以块体同性面与球锥对称轴平行或成小锐角时热应力最小。一般而言,工艺设计中应避免用模量大的主轴方向指向球锥对称轴方向。 相似文献
584.
A kind of wireless sensor was previously developed,which is powered and transmit signals wirelessly instead of using an electrical connection to the embedded reinforcement.Based on this technique,the relationship between diameters of corroded sensing steel wires and corrosion levels of steel bars is established by experiments.Quadratic function is utilized to fit the experiment results,and the correlation coefficients are all larger than 0.95.Estimated corrosion levels of commonly used steel bars are given for different diameters of corroded sensing steel wires fractured due to corrosion. 相似文献
585.
LIU Hua YANG Jia-ling LIU Kai-xin 《中国航空学报》2007,20(3):210-214
Theoretical analysis and numerical calculations of Love wave propagation in layered graded composites with imperfectly bonded interface are described in this paper. On the basis of WKB method, the approximate analytic solutions for Love waves are obtained. By the interface shear spring model, the dispersion relations for Love waves in layered graded composite structures with rigid, slip, and imperfectly bonded interfaces are given, and the effects of the interface conditions on the phase velocities of Love waves in SiC/Al lay- ered graded composites are discussed. Numerical analysis shows that the phase velocity decreases when the defined flexibility parameter is greater. For the general imperfectly bonded interface, the phase velocity changes in the range of the velocities for the rigid and slip interface conditions. 相似文献
586.
Three-dimensional computational fluid dynamics analyses have been employed to study the compressible and turbulent flow of the shock train in a convergent–divergent nozzle. The primary goal is to determine the behavior, location, and number of shocks. In this context, full multi-grid initialization, Reynolds stress turbulence model (RSM), and the grid adaption techniques in the Fluent software are utilized under the 3D investigation. The results showed that RSM solution matches with the experimental data suitably. The effects of applying heat generation sources and changing inlet flow total temperature have been investigated. Our simulations showed that changes in the heat generation rate and total temperature of the intake flow influence on the starting point of shock, shock strength, minimum pressure, as well as the maximum flow Mach number. 相似文献
587.
Chen Dong Yuming Fu Guanghui Liu Hong Liu 《Advances in Space Research (includes Cospar's Information Bulletin, Space Research Today)》2014
Minimizing energy consumption and maximizing crop productivity are major challenges to growing plants in Bioregenerative Life Support System (BLSS) for future long-term space mission. As a primary source of energy, light is one of the most important environmental factors for plant growth. The purpose of this study is to investigate the effects of low light intensity at different stages on growth, pigment composition, photosynthetic efficiency, biological production and antioxidant defence systems of wheat (Triticum aestivum L.) cultivars during ontogenesis. Experiments were divided into 3 intensity-controlled stages according to growth period (a total of 65 days): seedling stage (first 20 days), heading and flowering stage (middle 30 days) and grain filling stage (last 15 days). Initial light condition of the control was 420 μmol m−2 s−1 and the light intensity increased with the growth of wheat plants. The light intensities of group I and II at the first stage and the last stage were adjusted to the half level of the control respectively. For group III, the first and the last stage were both adjusted to half level of the control. During the middle 30 days, all treatments were kept the same intensity. The results indicated that low-light treatment at seedling stage, biomass, nutritional contents, components of inedible biomass and healthy index (including peroxidase (POD) activity, malondialdehyde (MDA) and proline content) of wheat plants have no significant difference to the control. Furthermore, unit kilojoule yield of group I reached 0.591 × 10−3 g/kJ and induced the highest energy efficiency. However, low-light treatment at grain filling stage affected the final production significantly. 相似文献
588.
The application of computational fluid dynamics/computational solid method (CFD/CSM) on solving the aero-thermo-elastic problem of spinning rocket is introduced. Firstly, the aerodynamic coefficients of a rocket are calculated, and the results are compared with the available experimental data, which verified the accuracy of the CFD output. Then, analysis is carried using ANSYS Workbench multi-physics coupling platform, which includes fluid, thermal, and structural solvers. The results show that spinning causes a significant effect on the de formations and stresses. Furthermore, thermal stresses due to high temperature at the rocket warhead and tail edges have a dominated effect, even more than those produced by aerodynamic forces. Consequently, this important outcome should be taken into consideration during the rocket design stages. 相似文献
589.
590.
Based on the complex variable method, the analytical solutions of stress functions and stress intensity factors(SIFs) are provided for the plane problem of two collinear edge cracks emanating from an elliptical hole in an infinite plate under shear. The stress distribution along the horizontal axis is given in graphical forms, which conforms to Saint-Venant's principle. The influences of crack length and ellipse shape on the stress intensity factors are evaluated. Comparing the analytical solutions with finite element method(FEM) results shows good coincidence. These numerical examples show that the present solutions are accurate. 相似文献