全文获取类型
收费全文 | 91篇 |
免费 | 64篇 |
国内免费 | 18篇 |
专业分类
航空 | 123篇 |
航天技术 | 4篇 |
综合类 | 12篇 |
航天 | 34篇 |
出版年
2023年 | 6篇 |
2022年 | 10篇 |
2021年 | 8篇 |
2020年 | 8篇 |
2019年 | 9篇 |
2018年 | 2篇 |
2017年 | 7篇 |
2016年 | 5篇 |
2015年 | 1篇 |
2014年 | 8篇 |
2013年 | 6篇 |
2012年 | 6篇 |
2011年 | 6篇 |
2010年 | 4篇 |
2009年 | 5篇 |
2008年 | 5篇 |
2007年 | 4篇 |
2006年 | 4篇 |
2005年 | 2篇 |
2004年 | 7篇 |
2002年 | 4篇 |
2001年 | 5篇 |
2000年 | 4篇 |
1999年 | 2篇 |
1998年 | 2篇 |
1997年 | 11篇 |
1996年 | 6篇 |
1995年 | 11篇 |
1994年 | 8篇 |
1993年 | 1篇 |
1992年 | 3篇 |
1990年 | 1篇 |
1989年 | 1篇 |
1987年 | 1篇 |
排序方式: 共有173条查询结果,搜索用时 15 毫秒
161.
孔凡荣%游敏%郑小玲%杨春梅 《宇航材料工艺》2004,34(4):39-43
运用弹塑性有限元法结合实验研究了连续和间隙连接的单搭接接头应力分布规律,并考虑了胶瘤的影响。结果表明,在相当大间隙长度范围内和适当的间隙位置条件下,间隙连接接头并没有大幅度地减小其承载能力,相反其有效搭接区域剪切强度呈明显升高趋势;胶层应力峰值仍然发生在搭接末端;胶瘤承担了相当大的载荷作用;过大的间隙长度以及不当的间隙位置会导致胶层靠近间隙端应力集中明显加剧,成为新的高应力区,可能导致接头破坏模式的改变。实验结果与数值分析结果很好地吻合。 相似文献
162.
复合结构喷管热强度有限元分析 总被引:3,自引:0,他引:3
本文采用有限元法对复合结构喷管进行了二维瞬态温度场和应力场计算。在温度场计算中采用了网络变换法对考虑烧蚀动边界并有效地消除了大温度梯度情况下温度振荡现象,算例表明,本文提供的分析方法简单可靠,易于工程实践采用。 相似文献
163.
时效前对Al-Li-Cu-Mg-Zr(2091)合金进行冷轧和温轧关系,用慢应变速率拉伸试验研究了合金在3.5%NaCl溶液中的应力腐蚀敏感生。结果表明,预轧制变形提高了合金的应力腐蚀抗力。冷轧受形量为20%以及温轧温度为180℃时,合金都具有最低的应力腐蚀敏感性。对合金应力腐蚀抗力与显微组织的关系进行了探讨。 相似文献
164.
固体火箭发动机的概率设计 总被引:2,自引:0,他引:2
固体火箭发动机的性能参数和结构参数一般都服从正态分布,利用应力-强度干涉理论,通过正态分布密度函数的耦合方程进行发动机结构设计,并推导出具有随机变量指数的发动机工作压强和燃烧室壳体弹塑性爆破压的均值和标准偏差表达式,导出传统安全系数与可靠概率的关系。该设计方法较之传统的采用安全系数的设计方法合理。 相似文献
165.
166.
167.
Understanding stress corrosion cracking behavior of 7085-T7651 aluminum alloy in polluted atmosphere
《中国航空学报》2023,36(8):408-421
The electrochemical and Stress Corrosion Cracking (SCC) behaviors of 7085-T7651 aluminum alloy in different environments are studied by electrochemical and mechanical testing. The research shows that the type, concentration of the corrosive medium and electrolyte state affect the electrochemical and SCC controlling processes of aluminum alloys. The Thin Electrolyte Layer (TEL) state and the addition of HSO3– increase the corrosion rate and SCC susceptibility. The presence of HSO3– in a corrosive environment can significantly accelerate the corrosion rate and mechanical property degradation, and this effect increases with the increase of HSO3– concentration. Compared with the solution environment, the TEL environment will further aggravate corrosion and mechanical property degradation. With the increase of HSO3– concentration, the pH of the corrosive environment exhibits little change, while the SCC degradation is significantly promoted. This is attributed to the HSO3– induced buffer effect and film-assisted stress effect, yielding the overshadowing effect against solution pH. 相似文献
168.
《中国航空学报》2023,36(2):304-315
This paper experimentally studied the stress corrosion behavior of 2195-T8 Al-Li alloys with prefabricated pits in 30vol% HNO3. The microstructure was observed and determined by the scanning electron microscopy and the transmission electron microscopy. The typical corrosion features, i.e., regular or irregular corrosion pits and sub/intergranular corrosion, were investigated, and the role of stress were analyzed. The statistical results of the number and area of corrosion pits in various sizes were studied using an improved image processing method. Experimental results demonstrate that stress affects the intergranular corrosion or sub-intergranular corrosion of the alloy most, and promotes them to evolve into cracks under stress corrosion. Stress also plays a role in accelerating corrosion severity of certain corrosion feature. The number of corrosion pits with an area of 0–50 μm2 can be seen as an index to reflect the degree of corrosion. Besides, a corrosion phenomenon, i.e., the pit bottom in the site with the maximum stress locally suffering from no severe corrosion, was observed and discussed. 相似文献
169.
李真 《民用飞机设计与研究》2013,(Z2)
介绍了角元法、切割法和板元法三种飞机结构型材压损的计算方法。采用切割法和板元法对某型飞机机身长桁压损试验件进行了计算,结果表明切割法和板元法均为偏保守的计算方法,切割法偏保守4%以上,板元法偏保守11%以上。切割法的计算结果更接近试验结果,为提高机体结构效率,减轻结构重量,建议采用切割法进行工程计算。 相似文献
170.
《中国航空学报》2023,36(8):182-206
For the stress-constrained topology optimization of a turbine disk under centrifugal loads, the jagged boundaries of the mesh and the gray densities on the solid/void interfaces could make the calculated stress field inconsistent with the actual value. It may result in overestimating the maximum stress and thus affect the effectiveness of stress constraints. This paper proposes a new method for predicting the maximum stress to overcome the difficulty. In the process, a predicted density is newly defined to obtain stable boundaries with thin layers of gray elements, a transition factor is innovatively proposed to evaluate the effects of intermediate-density elements, two different stiffness penalty schemes are flexibly used to calculate the elastic modulus of elements, and a linear stress penalty is further adopted to relax the stress field of the structure. The proposed approach for predicting the maximum stress value is verified by the analysis of a structure with smooth boundaries and the topology optimization of a turbine disk. An updating scheme of the stress constraint in the topology optimization is also developed using the predicted maximum stress. Some key ingredients affecting the optimization results are discussed in detail. The results prove the effectiveness and efficacy of the proposed maximum stress prediction and developed stress constraint methods. 相似文献