Constitutive behavior and microstructural evolution in hot deformed 2297 Al-Li alloy

The microstructural evolution mechanism and constitutive behavior of 2297 Al-Li alloy were studied via thermal compression test with the constant strain rates of 0.001–1 s⁻¹ and the deformation temperatures ranging from 623 to 773 K. To verify the predictable ability of diverse constitutive models under different stress states, the hot compression experiments with stress triaxiality varying from −0.33 to 0.46 were conducted. The microstructures of the deformed specimens under diverse deformation conditions are probed to reveal the mechanism of hot deformation behavior. The experimental results indicate that the work-hardening and dynamic softening are competitive during the hot compression process, and the dynamic softening is more obvious under low deformation temperature and high strain rate. The microstructural analysis manifests that the dynamic recovery gets predominant at high deformation temperature to produce fine grains. Meanwhile, the dynamic recrystallization becomes more dominant as the strain rate decreases, which is sensitive to the stress triaxiality. In addition, both the modified Johnson-Cook model and strain-compensated Arrhenius-type function are suitable for describing the flow behavior of 2297 alloy, while the latter reveals a more accurate prediction. However, the predictability of the two kinds of models is worsened with the transformation of stress triaxiality, and the validity of the Arrhenius-type model is restricted by high stress triaxiality.     

Revealing the hot intergalactic medium with ROSAT

The X-ray background intensity around galaxies and rich clusters of galaxies is investigated in three energy bands using the ROSAT All-Sky Survey maps. It is found that an amplitude of the XRB enhancements surrounding the Abell clusters and high density areas in the Lick galaxy counts depends on photon energy. Excess flux generated in the surrounding of the galaxy concentrations is consistent with the thermal emission by hot gas postulated by hydrodynamic simulations.     

喷管偏转对航空发动机特性影响的试验

通过整机地面试验的方法,对喷管偏转后发动机不同工作状态下各参数的分析,获得了矢量偏转时发动机推力损失、偏转效率、发动机工作特性变化等数据.试验结果表明:在相同高压转速下,随着几何矢量角的增大,发动机的推力损失增大,偏转效率先增大后减小;在相同几何矢量角下,随着转速的增加,发动机推力损失经历由增大到减小的过程,矢量喷管的偏转效率增大,但偏转效率均小于1;节流状态时发动机转速差随着几何矢量角的增大而增大,中间状态时发动机转速差不受几何矢量角的影响;发动机节流状态时的矢量偏转使风扇工作线上移,风扇裕度减小,工程应用中需考虑扩稳措施.      

高超声速飞行器控制面热防护技术跟踪研究

简要介绍了高超声速飞行器控制面的气动热环境特点,在此基础上,从热管理的角度对各种类型的热防护方案分别进行分析,论证了高超声速飞行器控制面采用热结构方案的合理性;并对高超声速飞行器控制面热结构方案的特点和进展、改进热结构的途径进行了综述和分析。     

基于“工作过程”机务实训的教学质量评价体系

分析广州民航职业技术学院机务实训教学质量评价体系存在的问题,提出如何基于工作过程构建一个全面合理的实训教学质量评价体系的原则和内容,并分析工作过程的质量评价体系的重要意义。     

Individual Differences in Representational Precision Predict Spatial Working Memory Span

Perhaps the signature feature of working memory is that it is limited. In the same subjects, we used two different retrieval tasks to independently measure two different limits of spatial memory. Precision was measured by asking participants to localize a missing target item among a field of other targets and distracters. Capacity was measured with a similar task where participants identified, rather than localized, a set of remembered targets from within a larger set of identical items. Across participants, the precision of localization was positively correlated with the number of successfully retrieved items. These data suggest that an individual's representational capacity may ultimately be constrained by their ability to form precise representations of space.     

抗坠毁座椅吸能装置的性能参数选择方法研究

决定抗坠毁座椅性能的主要参数是吸能装置的启动载荷及行程。本文针对确定吸能装置性能参数的方法进行了研究。     

单相流体回路工质的优选研究

流体工质的选择是单相流体回路设计的一项重要内容,文章概述了流体工质的基本性能参数与选择标准,简要介绍了单相流体回路的分析计算过程,提出了能初步衡量工质优劣的一个特征性能参量热耗比F,设定3种工况条件,分别绘制了6种工质的热耗比F随温度的变化曲线,将比较结果应用于一个流体双回路系统的内回路,在SINDA/FLUINT中建立数值仿真模型,计算结果显示利用热耗比F可以对流体工质进行初步的优选。     

Studying the evolution of the hot universe with the X-ray evolving universe spectroscopy mission – XEUS

Europe is one of the major partners building the International Space Station (ISS) and European industry, together with ESA, is responsible for many station components including the Columbus Orbital Facility, the Automated Transport Vehicle, two connecting modules and the European Robotic Arm. Together with this impressive list of contributions there is a strong desire within the ESA Member States to benefit from this investment by utilizing the unique capabilities of the ISS to perform world-class science. XEUS is one of the astronomical applications being studied by ESA to utilize the capabilities of the ISS. XEUS will be a long-term X-ray observatory with an initial mirror area of 6 m² at 1 keV that will be expanded to 30 m² following a visit to the ISS. The 1 keV spatial resolution is expected to be 2–5″ half-energy-width. XEUS will consist of separate detector and mirror spacecraft (MSC) aligned by active control to provide a focal length of 50 m. A new detector spacecraft, complete with the next generation of instruments, will also be added after visiting the ISS. The limiting 0.1–2.5 keV sensitivity will then be 4 × 10⁻¹⁸ erg cm⁻² s⁻¹, around 200 times better than XMM-Newton, allowing XEUS to study the properties of the hot baryons and dark matter at high redshift.     

多级涡轮多工况气动优化设计研究

采用将准三维设计和多级局部优化联合的多级涡轮多工况气动优化设计流程对某三级航空发动机涡轮进行多级气动优化设计.优化联合采用人工神经网络和遗传算法对各列叶栅进行三维局部优化,流场计算采用全三维粘性流N-S方程求解.通过优化设计,改善了各列的性能,并对各列间参数进行了优化匹配,两种工况的总效率均提高1%,总流量基本不变,总体性能提高,达到设计要求.