Fatigue crack growth in SiC particulates reinforced Al matrix graded composite

The SiC/Al graded composite was fabricated by powder metallurgy processing and its fatigue crack growth behavior was studied. The volume percentage of SiC particulates was distributed from 5 to 30% layer by layer on the cross section. Since the aluminium was dissolved together, there was no evident interface between the two layers with different volume fraction of SiC particulates. Fatigue crack growth was in direction of from 5 to 30% SiC layers under sinusoidal wave-form. The retardation of fatigue crack growth was found when crack propagated from low volume fraction of SiC to high volume fraction of SiC. The crack deflection and branching between two layers were observed, which decreased crack growth rates. In view of crack tip driving force, the plasticity mismatch between the layers shielded crack tip driving force, i.e. decreased the effective J-integral at the tip of the crack as the plastic zone of the crack tip spread from the weaker material into the stronger material.     

水量还原方法及合理性检查

文中详细地阐述了取河水、井水、水库水、跨流城引(排)水等不同情况进行还原的具体方法步骤。并对水量还原成果提出合理性检查措施。     

灌浆技术在紫山灰坝迎灰坡裂缝处理中的应用

本文分析了紫山灰坝迎灰坡裂缝的成因，并介绍了充填式灌浆处理方法，效果良好。     

激光熔覆专用铁基合金粉末的研究进展

指出了目前防止熔覆层开裂所采取的主要措施中存在的问题,阐述了激光熔覆和热喷涂对于所用合金粉末性能要求之异同,评述了激光熔覆专用铁基合金粉末的研制现状,提出了成分与组织设计的新思想。     

Fatigue limit evaluation of notches,small cracks and defects: an engineering approach

In this paper, the average stress method for the fatigue limit evaluation of stress raising geometrical features is revised and extended. In particular, an analytical close‐form approach was used and the linear elastic stress equations were modified by taking into account the effect of nominal stress on the local stress distribution. Hence, the average tangential stress was correctly evaluated over a distance of 2a₀, where a₀ was El Haddad's short crack constant, for long and small notches as well as for crack‐like notches. When this model is applied to a wide range of geometrical features subjected to mode I fatigue loading, the classical shape of the curves of the Kitagawa–Takahashi diagram was obtained for changes in crack‐like notch size. Similarly, notch sensitivity was estimated by reducing the notch tip radius. The accuracy of the proposed method in predicting fatigue limits was then checked by using experimental data taken from the literature and generated on testing specimens weakened by rounded and sharp notches as well as by small artificial defects.     

黄河口河道演变规律探讨

通过分析黄河口河道在纵剖面、横断面、河型等方面的演变过程,总结归纳出黄河口河道的演变规律。指出:黄河口泥沙在潮汐涨落等因素影响下,河口河道纵剖面逐渐形成台阶状,与此同时,河口滩地横比降逐渐发展为倒比降;河口河道中段由顺直型河道逐渐转为弯曲型河道,而下段仍为相对顺直、游荡型河道。当河口河道中段比降减小到一定程度后,此河段开始漫滩、卡冰、出汊。河口台阶的形成揭示了黄河口流路由单股河道逐渐转为出汊的过程,即黄河口流路由“青壮期”逐渐转为“衰亡期”的过程。延长黄河口流路使用年限的途径是:①尽量减少黄河下游输向黄河口的泥沙量;②采取河口挖沙或人工改汊措施,地点宜选在河口河道的中下段。     

永升城基础大体积混凝土施工的裂缝预控

基础大体积混凝土施工的裂缝控制 ,从分析产生裂缝的原因来阐述 ,将冷缝作为结构性裂缝来预控     

中扬子及邻区层序地层与原型盆地演化

中扬子及邻区原型盆地可划分为 9个大层序,其中,1～6大层序由中、古生代海相地层组成;第 7大层序为早、中侏罗纪的陆相沉积;第 8大层序为晚侏罗世的前渊沉积;第 9层序为晚白垩世至第三纪的伸展盆地。震旦纪,中部地区为台地相环境,向南为浅海陆棚环境,向北以陆表海为主;寒武纪至早奥陶世为典型的大陆边缘盆地;中、晚奥陶世至志留纪为裂谷盆地发展阶段;泥盆纪至石炭纪该区发生广泛海侵,与华南海域和太平洋海域多处相连;二叠纪至早、中三叠世为原型盆地的重要转型时期,随着分隔秦岭微板块与扬子板块的勉略古洋盆向东打开,扬子北缘由前期的区域性隆起转变为向北加深的大陆边缘盆地;晚三叠世经历了两次幕式旋回,巴东组沉积时期盆地沉降缓慢,九里岗组沉积时期则较快;早、中侏罗世原型盆地早幕 (早侏罗世)沉积缓慢,晚幕 (中侏罗世)快速沉降,以水下沉积作用为主;晚侏罗世可划分为两大构造演化阶段,早期构造活动相对平静,晚期强烈;晚白垩世至老第三纪,盆地范围缩小,以湖泊、河流体系为主。由此,中扬子及邻区在地质历史时期经历了 4种不同性质的原型盆地,具有幕式充填特征。     

On the corrosion fatigue crack initiation model and expression of metallic notched elements

In the present study, attempts are made to extend the application of the mechanical model for the fatigue crack initiation (FCI) and the FCI life formula of metallic notched elements in laboratory air to those in the corrosive environment. The test results and analysis of the corrosion FCI (CFCI) life of aluminum alloys and Ti---6A1---4V show that the expression of the CFCI life obtained by modifying the FCI life formula in laboratory air can give a good fit to the test results of the CFCI life. The salt water (3.5% NaCl) environment has no effects on the CFCI resistant coefficient compared with the FCI resistant coefficient in laboratory air. However, 3.5% NaCl environment greatly decreases the CFCI threshold of aluminum alloy, but has little effect on the CFCI threshold of Ti---6A1---4V. The loading frequency ranging from 1 Hz to 10 Hz has no appreciable effect on the CFCI life, and thus, the CFCI threshold of aluminum alloys investigated. Hence, the expression for the CFCI life of metallic notched elements proposed in this study is a better one, which reveals a correlation between the CFCI life and the governing parameters, such as, the geometry of the notched elements, the nominal stress range, the stress ratio, the tensile properties and the CFCI threshold. However, this new expression of the CFCI life needs to be verified by more test results.     

STRESS INTENSITY FACTORS AND WEIGHT FUNCTIONS FOR SEMI-ELLIPTICAL SURFACE CRACKS IN FINITE-THICKNESS PLATES UNDER TWO-DIMENSIONAL STRESS DISTRIBUTION

Abstract— A Fourier series approach is proposed to calculate stress intensity factors using weight functions for semi-elliptical surface cracks in flat plates subjected to two-dimensional stress distributions. The weight functions were derived from reference stress intensity factors obtained by three-dimensional finite element analyses. The close form weight functions derived are suitable for the calculation of stress intensity factors for semi-elliptical surface cracks in flat plates under two-dimensional stress distributions with the crack aspect ratio in the range of 0.1 ≤ a/c ≤ 1 and relative depth in the range of 0 ≤ a/t ≤ 0.8. Solutions were verified using several two-dimensional non-linear stress distributions; the maximum difference being 6%.