大体积混凝土施工与裂缝控制--万信城市花园B区高层住宅

石家庄市万信城市花园B区高层住宅楼筏板基础大体积混凝土连续浇注施工,采取有效技术措施控制温度裂缝,未产生结构有害的裂缝,取得了很好的技术与经济效益.     

如何在应用软件中实现财务数学公式自定义

本文实现了在开发具有数据校验功能的软件时,一种全新的数据校验方法,将传统的写在程序中的校验公式或利用手工进行检验数据的方式完全抛弃.该种方法具有配置灵活、维护简单和功能强大的特点,利用界面元素命名方法,内置校验公式到各个界面元素中,而公式是可以灵活维护的,一般是将公式存贮在数据库表中,在软件需校验数据时,从数据库表中读取公式,根据公式中涉及到的各种界面数据项进行自动的数据校验并得出校验结果.这对需大量数据校验和校验算法经常改变的软件是非常有用的.     

Study of ionospheric D region changes during solar flares using MF radar measurements

During solar flares, the X-ray radiation suddenly increases, resulting in an increase in the electron density of the atmospheric D region and a strong absorption of short-wave radio waves. Based on Langfang medium frequency (MF) radar, this paper analyzed the variation characteristics of D region in the lower ionosphere from 62 km to 82 km. The analysis focused on multiple C-level and M-level solar flare events before and after the large-scale flare event at 11:53 (UT) on September 6, 2017. The results show that it is difficult to detect the electron density over 70 km in Langfang during solar flares, but the electron density value can be obtained as low as 62 km, and the stronger the flare intensity, the lower the detectable electron density height. Besides, the equal electron density height, the received power of X and O waves will also be significantly reduced during the flares, and the reduction of equal electron density height has a weak linear relationship with flare intensity.     

某航天器输氢管道系统结构完整性评估

为保障某航天器在服役年限内不发生事故，针对航天器上采用插入焊接技术的精密管道系统进行结构完整性评估。在考虑到系统存在整圈的环形未焊透缺陷基础上，结合工程实践，假设在焊接区域存在更危险的平面缺陷。首先，开展高压气相热充氢试验下的标准拉伸和三点弯试验得到管道系统材料"J-75"在临氢环境下应力应变曲线和断裂韧性。其次，采用有限元程序计算系统在内压、惯性载荷与离面位移作用下的应力分布，考虑到间隙配合中的不确定性，改变模型中的最大间隙多次模拟计算，发现最大应力位置基本不变，以此区域作为假想缺陷的具体萌生区域。最后，采用失效评估图（FAD）方法对存在4种缺陷模式的系统分别进行结构完整性评估。通过引入安全裕度的概念，发现系统在含有初始尺寸（0.15 mm）的4种平面缺陷时，均处于安全状态，并且安全裕度都在2倍以上；通过工程临界分析（ECA）发现随着缺陷尺寸的增大，系统中含有缺陷2（位于管道焊接区域最大应力处的轴对称平面且沿焊深方向扩展的缺陷）时最为危险，且当缺陷深度超过0.61 mm时将断裂失效；考虑到测试数据的弥散性，针对系统最危险的模式，以安全裕度为可靠性指标，将失效评估图方法与可靠性评价相结合，得到系统在含有尺寸为0.15 mm的缺陷2情况下保有足够安全裕度的可靠性下限值超过0.999 5。     

Parametric Modeling of Circuit Model for AC Glow Discharge in Air

In the parametric modeling of the circuit model for glow discharge in air,a new method for the design of glow discharge circuit model is presented.The new circuit model is an important reference for the design of plasma power supply,the simulation of glow discharge plasma actuator and the simulation of glow discharge plasma anemometer.The modeling approach consists in developing an electrical model of the glow discharge in air based on circuit components.The structure of the circuit model is established according to the theoretical analysis and the experimental device.Then the parameters of the circuit model are obtained based on the circuit analysis.Finally,the circuit model is verified by comparing the simulation current with the experimental current.This model takes into account the whole framework of the air glow discharge including the sheath and the plasma area.The built circuit model is feasible and reliable,thus being instructive for the investigation of the glow discharge in air.     

Focus Reflective Shock Wave Interaction with Flame

An experiment on deformation of flame under the effect of focusing shock wave reflection is performed with the help of multiple-spark camera to understand the flame instability of the deformation process. Methane and oxygen are mixed stoichiometrically to be used in the experiment. Based on Navier-Strokes equations, two-dimen- sional axisymmetric elementary reactions are numerically simulated. And the simulation results are solved by opti- cal calculation. Shaded pictures by simulation fit well with experimental photos. Focusing reflecton shock waves can affect the flame, which accelerates the deformation of flame and renders violent burning in high-energy flam- mable gases behind waves. Therefore anticlockwise whirlpool appears. It clusters around the external surface of flame and has a tendency to develop toward the right. Finally, the whirlpool focuses on the right side of the flame, which involves the fresh unfired gases into the whirlpool circle, and consequently the head of mushroom cloud is formed. Meanwhile, when shock wave passes through the flame, the intensity of the shock waves on the axis is strengthened.     

DZ22B高温合金定向凝固叶片铸造缺陷的形成机理研究

采用SEM、EDS等分析手段研究了DZ22B镍基高温合金定向凝固涡轮叶片不同区域铸造缺陷的特点及其形成原因。结果表明,裂纹缺陷主要分布在叶身的中上部位,其形成机理主要归因于叶片在凝固过程中的共晶组织过多;而疏松缺陷分布在叶身和缘板部位,产生在枝晶间共晶组织附近。枝晶间距小补缩不足和反应生成的CO气体未及时排除是疏松形成的两大原因。     

捆绑火箭POGO振动动力学模型的研究

确定了捆绑火箭POGO振动动力学模型中蓄压器的最佳安装位置,简化了液体捆绑火箭动力学模型。基于AMESim软件搭建捆绑火箭动力学仿真模型,分析了蓄压器的安装位置对捆绑火箭POGO振动系统的系统阻尼比的影响,以及贮箱、直管、泵和推力室产生的作用力对系统阻尼比的影响。结果表明:蓄压器安装在芯级氧路和助推氧路的系统阻尼比提升最大,POGO振动的抑制效果最好;推力室产生的作用力对系统阻尼比的影响占主导地位,故仅需考虑推力室产生的作用力,以简化捆绑火箭POGO振动动力学模型。该研究可应用于POGO振动的仿真过程。     

海洋大气环境下微动开关触点回跳时间增大故障的试验复现与分析

结合某型微动开关触点回跳时间增大导致某系统故障问题,设计了由干湿交替酸性盐雾试验和湿热试验组成的海洋大气环境效应加速模拟试验剖面,选取与外场故障件型号一致的微动开关为研究对象,通过实验室加速模拟试验,成功复现了外场故障现象,并结合试验结果对腐蚀性环境、电烧蚀等因素对触点回跳时间增大的影响机制进行了分析。