全文获取类型
收费全文 | 365篇 |
免费 | 27篇 |
国内免费 | 75篇 |
出版年
2023年 | 2篇 |
2021年 | 8篇 |
2019年 | 6篇 |
2018年 | 9篇 |
2017年 | 26篇 |
2016年 | 29篇 |
2015年 | 8篇 |
2014年 | 24篇 |
2013年 | 24篇 |
2012年 | 34篇 |
2011年 | 32篇 |
2010年 | 13篇 |
2009年 | 38篇 |
2008年 | 19篇 |
2007年 | 26篇 |
2006年 | 47篇 |
2005年 | 31篇 |
2004年 | 22篇 |
2003年 | 15篇 |
2002年 | 4篇 |
2001年 | 4篇 |
2000年 | 8篇 |
1999年 | 12篇 |
1998年 | 5篇 |
1997年 | 4篇 |
1996年 | 6篇 |
1995年 | 2篇 |
1994年 | 5篇 |
1993年 | 1篇 |
1992年 | 1篇 |
1991年 | 1篇 |
1990年 | 1篇 |
排序方式: 共有467条查询结果,搜索用时 0 毫秒
461.
462.
463.
破片式战斗部对空中飞机的毁伤建模与仿真 总被引:2,自引:0,他引:2
研究了破片式战斗部对空中飞机的易损性分析方法、目标毁伤树的基本结构和关键部件的毁伤准则。通过对空中飞机关键部件的简化和对破片与关键部件的交汇分析,建立了破片式毁伤元作用下空中飞机易损性分析计算模型,并运用MATLAB计算仿真软件研究了破片式战斗部作用下空中飞机在不同炸点和不同交汇条件下的毁伤效能分析。 相似文献
464.
465.
466.
De-icing technology has become an increasingly important subject in numerous applications in recent years. However, the direct numerical modeling and simulation the physical process of thermo-mechanical deicing is limited. This work is focusing on developing a numerical model and tool to direct simulate the de-icing process in the framework of the coupled thermo-mechanical peridynamics theory. Here, we adopted the fully coupled thermo-mechanical bond-based peridynamics (TM-BB-PD) method for modeling and simulation of de-icing. Within the framework of TM-BB-PD, the ice consti-tutive model is established by considering the influence of the temperature difference between two material points, and a modified failure criteria is proposed, which takes into account temperature effect to predict the damage of quasi-brittle ice material. Moreover, thermal boundary condition is used to simulate the thermal load in the de-icing process. By comparing with the experimental results and the previous reportedfinite element modeling, our numerical model shows good agreement with the pre-vious predictions. Based on the numerical results, we find that the developed method can not only predict crack initiation and propagation in the ice, but also predict the temperature distribution and heat conduction during the de-icing process. Furthermore, the influence of the temperature for the ice crack growth pattern is discussed accordingly. In conclusion, the coupled thermal-mechanical peridynamics formulation with modified failure criterion is capable of providing a modeling tool for engineering ap-plications of de-icing technology. 相似文献
467.
To deal with the radio frequency threat posed by modern complex radar networks to aircraft, we researched the unmanned aerial vehicle (UAV) formations radar countermeasures, aiming at the solution of radar jamming resource allocation under system countermeasures. A jamming resource allocation method based on an improved firefly algorithm (FA) is proposed. Firstly, the comprehensive factors affecting the level of threat and interference efficiency of radiation source are quantified by a fuzzy comprehensive evaluation. Besides, the interference efficiency matrix and the objective function of the allocation model are determined to establish the interference resource allocation model. Finally, A mutation operator and an adaptive heuristic are integtated into the FA algorithm, which searches an interference resource allocation scheme. The simulation results show that the improved FA algorithm can compensate for the deficiencies of the FA algorithm. The improved FA algorithm provides a more sci-entific and reasonable decision-making plan for aircraft mission allocation and can effectively deal with the battlefield threats of the enemy radar network. Moreover, in terms of convergence accuracy and speed as well as algorithm stability, the improved FA algorithm is superior to the simulated annealing algorithm (SA), the niche genetic algorithm (NGA), the improved discrete cuckoo algorithm (IDCS), the mutant firefly algorithm (MFA), the cuckoo search and fireflies algorithm (CSFA), and the best neighbor firefly algorithm (BNFA). 相似文献