全文获取类型
收费全文 | 193篇 |
免费 | 92篇 |
国内免费 | 19篇 |
出版年
2024年 | 1篇 |
2023年 | 2篇 |
2022年 | 7篇 |
2021年 | 9篇 |
2020年 | 9篇 |
2019年 | 5篇 |
2018年 | 5篇 |
2017年 | 15篇 |
2016年 | 18篇 |
2015年 | 12篇 |
2014年 | 16篇 |
2013年 | 14篇 |
2012年 | 23篇 |
2011年 | 13篇 |
2010年 | 7篇 |
2009年 | 20篇 |
2008年 | 9篇 |
2007年 | 8篇 |
2006年 | 14篇 |
2005年 | 14篇 |
2004年 | 10篇 |
2003年 | 4篇 |
2002年 | 4篇 |
2001年 | 7篇 |
2000年 | 8篇 |
1999年 | 6篇 |
1998年 | 5篇 |
1997年 | 6篇 |
1996年 | 4篇 |
1995年 | 3篇 |
1994年 | 4篇 |
1993年 | 5篇 |
1992年 | 6篇 |
1991年 | 2篇 |
1990年 | 6篇 |
1989年 | 3篇 |
排序方式: 共有304条查询结果,搜索用时 15 毫秒
201.
The debris from exploded buildings can ricochet after colliding with the ground, thus increasing the debris travel distance and danger from any associated impacts or collisions. To reduce this danger, the travel distance of ricocheted debris must be accurately predicted. This study analyzed the change in the travel distance of ricocheted concrete debris relative to changes in the properties of a sand medium. Direct shear tests were conducted to measure the change in internal friction angle as a function of temperature and water content of the sand. Finite element analysis (FEA) was then applied to these variables to predict the speed and angle of the debris after ricochet. The FEA results were compared with results of low-speed ricochet experiments, which employed variable temperature and water content. The travel distance of the debris was calculated using MATLAB, via trajectory equations considering the drag coefficient. As the internal friction angle decreased, the shear stress decreased, leading to deeper penetration of the debris into the sand. As the loss of kinetic energy increased, the velocity and travel distance of the ricocheted debris decreased. Changes in the ricochet velocity and travel distance of the debris, according to changes in the internal friction angle, indicated that the debris was affected by the environment. 相似文献
202.
《防务技术》2022,18(9):1662-1678
In current guidelines, the free air blast loads (overpressure and impulse) are determined by spherical charges, although most of ordnance devices are more nearly cylindrical than spherical in geometry. This may result in a great underestimation of blast loads in the near field and lead to an unsafe design. However, there is still a lack of systematic quantitative analysis of the blast loads generated from cylindrical charges. In this study, a numerical model is developed by using the hydrocode AUTODYN to investigate the influences of aspect ratio and orientation on the free air blast loads generated from center-initiated cylindrical charges. This is done by examining the pressure contours, the peak overpressures and impulses for various aspect ratios ranged from 1 to 8 and arbitrary orientation monitored along every azimuth angle with an interval of 5°. To characterize the distribution patterns of blast loads, three regions, i.e., the axial region, the vertex region and the radial region are identified, and the propagation of blast waves in each region is analyzed in detail. The complexity of blast loads of cylindrical charges is found to result from the bridge wave and its interaction with primary waves. Several empirical formulas are presented based on curve-fitting the numerical data, including the orientation where the maximum peak overpressure emerges, the critical scaled distance beyond which the charge shape effect could be neglected and blast loads with varied aspect ratio in arbitrary orientation, all of which are useful for blast-resistant design. 相似文献
203.
介绍了高灵敏度空气采样感烟火灾探测系统的性能、结构特点及工作原理,并重点讨论了此系统在高大空间的应用。 相似文献
204.
针对机抖激光陀螺角随机游走和发动机干扰等影响静态捷联寻北精度的问题,提出了一种新的基于区间正交小波变换的前向线性预测算法。该算法利用前向线性预测技术以及区间正交小波变换抑制边界效应的能力,有效地减小了角随机游走和发动机干扰。车载实验证明该算法的有效性。 相似文献
205.
206.
207.
在大范围真实地形环境中规划出满足任务要求、导航、安全性等约束的较优航路,对提高无人机(UAV)的武器系统性能有重要意义。在基于直接航路编码的遗传算法中引入优化操作算子,将复杂约束合理地应用于遗传进化过程,可以较好地克服一般遗传操作的不足。采用均匀设计的试验方法确定较优的控制参数,并通过算例验证了算法的有效性。 相似文献
208.
在KD-03低速风洞中研制了一种附面层可人为地控制的均匀抽吸地板系统。在不同来流速度和不同抽吸系数条件下,对均匀抽吸地板上附面层速度分布进行了实验研究。实验结果与理论计算结果一致。在该地板上的高速列车模型风洞实验的结果与国外同类模型在移动带地板上的实验结果一致。利用均匀抽吸地板可有效地消除阻面层的影响,从而提高模型风洞实验气动力的试验精度。 相似文献
209.
研究了低入射余角下雷达海杂波的建模、仿真算法及实现问题。根据实际背景 ,对实测数据进行深入讨论 ,建立起一个较为准确的海杂波幅度分布模型与功率谱模型 ;针对非相参和相参两种雷达体制 ,分别采用修正的零记忆非线性变换法和球不变随机过程法来实现具有给定相关性的K分布随机数序列的产生 ,并以VisualC + +为平台实现了仿真软件。仿真结果证明了模型和算法的有效性。 相似文献
210.