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   363篇
  免费   1篇
公路运输   136篇
综合类   22篇
水路运输   126篇
铁路运输   66篇
综合运输   14篇
  2023年   9篇
  2022年   4篇
  2021年   29篇
  2020年   20篇
  2019年   4篇
  2018年   5篇
  2017年   6篇
  2016年   6篇
  2015年   14篇
  2014年   24篇
  2013年   17篇
  2012年   15篇
  2011年   24篇
  2010年   9篇
  2009年   9篇
  2008年   14篇
  2007年   20篇
  2006年   25篇
  2005年   20篇
  2004年   15篇
  2003年   9篇
  2002年   9篇
  2001年   8篇
  2000年   4篇
  1999年   6篇
  1998年   6篇
  1997年   8篇
  1996年   10篇
  1995年   4篇
  1994年   6篇
  1993年   2篇
  1992年   1篇
  1991年   2篇
排序方式: 共有364条查询结果,搜索用时 15 毫秒
61.
王霄锋  何泽民 《汽车工程》1994,16(3):149-154
本文结合基于局部应力-应变法疲劳寿命估算提出一种在“相对”意义上对野外实测应变信号进行删“小量”(即对疲劳影响不大的小信号分量)处理,获得用于室内随机疲劳试验的浓缩信号的方法,其中以损伤滞回环为删除单元,以相对疲劳损伤比为删除的门槛值。  相似文献   
62.
复杂载荷下曲轴疲劳强度的可靠性   总被引:1,自引:0,他引:1  
针对目前发动机曲轴疲劳可靠性设计方法法中存在的不足,通过对曲轴疲劳试验程序载荷谱及P-σ-N曲线的研究,提出出用程序载荷谱测定了P-σ-N曲线,并应用疲劳损伤等交理论对承受复杂载荷的贡轴进行可靠性设计的新方法。  相似文献   
63.
针对运营期高铁隧道衬砌结构在飞机降落冲击荷载作用下的动力响应规律及疲劳损伤问题,以成自高铁下穿天府机场东二跑道区间隧道为工程背景,采用有限元分析的方法研究隧道动力响应及疲劳损伤规律。结果表明:B747-400型飞机在粗暴着陆后0.05 s时刻动力载荷达到最大值,约为500 kN;在单次粗暴着陆工况下,拱顶位移和受力最大,位移最大峰值为1.58 mm,拉应力最大峰值为437.79 kPa,压应力最大峰值为556.24 kPa,衬砌结构未出现塑性损伤;飞机荷载长期作用下,随着循环次数的增加,结构损伤部位和程度也随之增加,拱顶损伤最突出,其次为边墙,隧道衬砌在上方飞机长期粗暴着陆作用下的疲劳寿命大致为25 a。  相似文献   
64.
In recent years, the dynamic responses of flexible risers have been the focus of many researchers. Most flexible risers undergo a substantial level of irregular motion from environmental loadings, which involves a continuous slip of helical wires. The slip of helical wires especially leads to a hysteretic effect by reducing the bending stiffness, making it hard to predict the dynamic responses of flexible risers. The current study, as an extension to Part I, presents a new large-scale dynamic analysis method for flexible risers. The suggested method creates a large-scale model for the dynamic analysis that considers a geometric and bending nonlinearity of flexible risers. The kinematics of each beam element is formulated based on a Green-Lagrangian strain and the interaction with the seabed, providing a realistic analysis of flexible risers. In particular, the current study introduces a direct moment correction method that modifies the internal force vector using an improved analytical model. The improved analytical model is assigned at each node of the large-scale model and estimates an accurate bending hysteresis curve considering the effect of shear deformation and varying tension. The suggested method corrects the bending moment and shear force of all beam elements based on the bending hysteresis curves obtained from the improved analytical model, by which a complex bending behavior of flexible risers is reflected in a large-scale domain. As a result, this study achieves a more accurate prediction of the dynamic responses and fatigue damage of flexible risers. A new dynamic analysis program, called OPFLEX, is developed herein based on the suggested analysis method. Using the developed program, the current study conducts several numerical investigations to identify the effect of the shear deformation and varying tension. Consequently, it is confirmed that the shear deformation of internal layers reduces the fatigue damage of helical wires by delaying the increase of internal stress. It is also identified that the effect of varying tension deteriorates the fatigue life of flexible risers through a continuous change of contact pressure during bending.  相似文献   
65.
针对乳化沥青冷再生作为路面下面层时适用公路等级的问题,拟定了9种典型的冷再生路面组合形式,运用BISAR3.0软件分析了不同厚度和基层模量的再生路面结构的路表弯沉值和疲劳寿命,结合工程实践和我国交通等级的划分,分析了不同厚度下冷再生面层适应的公路等级。  相似文献   
66.
疲劳驾驶检测方法的研究进展   总被引:1,自引:0,他引:1  
全世界每年因驾驶员疲劳驾驶而导致的死亡人数占交通灾难性事故的57%,故针对疲劳驾驶检测方法的研究具有现实意义.阐述了目前国内外各类疲劳驾驶检测方法的研究难点,介绍并对比分析了基于驾驶员生理参数、驾驶员行为特征、车辆行为特征的各类客观检测方法;最后对疲劳驾驶检测方法的发展趋势和应用前景进行了论述.  相似文献   
67.
焊接残余应力在焊接构件中普遍存在,直接影响车架结构的承载能力、降低焊接接头及整个车架构件的疲劳强度,在遇到外力作用时会产生疲劳断裂或脆性断裂而引发事故。只有从结构设计、工艺制造、焊后处理等阶段进行控制和消除,才能保证使用要求,提高焊接构件的强度,延长工作寿命。  相似文献   
68.
69.
In this study corrosion-fatigue tests have been conducted on fracture mechanics specimens extracted from an S355 G10+M structural steel welded plate. The tests have been performed on compact tension specimens with the crack tip located in the heat affected zone. The corrosion-fatigue test results from this study have been compared with the data available on the base metal as well as air tests on the same material. Moreover, the obtained results have been compared with the corrosion-fatigue data available in the literature on a wide range of steels and also the fatigue trends for welded joints in free-corrosion condition recommended in the BS7910 Standard. The effect of the specimen orientation, with respect to the weld region, is also examined in this study and it has been found that higher corrosion-fatigue crack growth rates are generally observed in the tests with 0° orientation. The results have also shown that the corrosive environment has significant effects on the fatigue crack growth acceleration at the beginning of the tests; however, as the crack propagates, the environmental damage effect on crack growth behaviour becomes less pronounced. The results presented in this study are discussed in terms of improvement in the structural integrity assessment of offshore wind turbine monopiles.  相似文献   
70.
The integrity of mooring chains is essential to the safety of a range of offshore platforms. However, mooring line failures are occurring earlier than their design lives, with a high number of these failures occurring due to fatigue. Early in the fatigue life of the component fatigue initiation processes occur, where the fatigue hotspot is sensitive to the mean load and there is plastic strain accumulation from the multiaxial stress-strain responses of the material, leading to cyclic plastic damage accumulation. The traditional SN approach suggested by mooring standards does not consider these effects, and it is proposed that this lack of consideration under low-cycle fatigue conditions is the reason for the current non-conservative fatigue assessments of mooring chains. This paper aims to develop a fatigue approach based on a critical plane multiaxial fatigue criterion for mooring chains that can consider the damage-induced by the cyclic plasticity and the mean load effect, to investigate the importance of incorporating low-cycle fatigue into the mooring chain life prediction. To develop the critical plane approach, the multiaxial stress-strain states are extracted for the critical plane at the fatigue hotspot from a finite element model of a mooring chain. This is then correlated with a fatigue life prediction provided by conventional fatigue design data. It uses a simulation of an FPSO as a case study to demonstrate the importance of low cycle fatigue, which shows that the mean load effect is significant in reducing the fatigue life for mooring chain applications, while the effect of fatigue damage-induced cyclic plasticity is limited. The fatigue damage accumulation predicted by the critical plane approach is significantly higher than that of the traditional SN approach and should be accounted for in mooring line design.  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