摘要：Due to the complex high-temperature characteristics of hydrocarbon fuel,the research on the long-term working process of parallel channel structure under variable working conditions,especially under high heat-mass ratio,has not been systematically carried *** this paper,the heat transfer and flow characteristics of related high temperature fuels are studied by using typical engine parallel channel *** numeri⁃cal simulation and systematic experimental verification,the flow and heat transfer characteristics of parallel chan⁃nels under typical working conditions are obtained,and the effectiveness of high-precision calculation method is preliminarily *** is known that the stable time required for hot start of regenerative cooling engine is about 50 s,and the flow resistance of parallel channel structure first increases and then decreases with the in⁃crease of equivalence ratio(The following equivalence ratio is expressed byΦ),and there is a flow resistance peak in the range ofΦ=0.5~*** is mainly caused by the coupling effect of high temperature physical proper⁃ties,flow rate and pressure of fuel in parallel *** the same time,the cooling and heat transfer character⁃istics of parallel channels under some conditions of high heat-mass ratio are obtained,and the main factors affect⁃ing the heat transfer of parallel channels such as improving surface roughness and strengthening heat transfer are *** the experiment,whenΦis less than 0.9,the phenomenon of local heat transfer enhancement and deterioration can be obviously observed,and the temperature rise of local structures exceeds 200℃,which is the risk of structural ***,the reliability of long-term parallel channel structure under the condition of high heat-mass ratio should be fully considered in structural design.

摘要：为解决低进气量条件下油气涡轮功率与效率提升困难的问题,本文结合裂解油气物性特点,针对性地提出了局部进气裂解油气向心涡轮设计方案。通过数值仿真详细分析了向心式油气涡轮在设计工况下的内部流动特征,并总结了非设计工况下轮周效率随压比、转速以及正癸烷裂解度的变化规律与影响机制。仿真结果表明,本文所设计油气涡轮在0.5 kg/s进气量条件下可实现38.8 kW功率输出,轮周效率为68%,能够满足油气涡轮气动设计需求。根据结果分析可知,随着压比的增大,轮周效率呈现出先增大后减小的趋势:低压比条件下轮周效率增大主要与转子入口攻角损失有关;高压比条件下轮周效率降低则主要是由于激波损失及其引发的附面层分离损失不断增大导致的。研究表明,轮周效率随转速、裂解度发生变化时与转子入口攻角有直接关系,其中,油气工质裂解度每提高20%,涡轮轮周效率可提高13%左右。

摘要：According to the modularization and standardization of program structure in Global/Regional Assimilation and Prediction System (GRAPES), the plug-compatible and transplantable regional meso-scale and global middle-range physics software package is established. The package's component integrality is comparative with the other advanced models physics. A three-level structure of connecting GRAPES physics and dynamic frame has been constructed. The friendly interface is designed for users to plug in their own physics packages. Phenomenon of grid-point storm rainfall in numerical prediction is analyzed with the numerical tests. The scheme of air vertical velocity calculation is improved. Optimizing tests of physics schemes are performed with the correlative parameters adjusting. The results show that the false grid-point storm rainfall is removed by precipitation scheme improving. Then the score of precipitation forecast is enhanced.

摘要：为结合当前针织服装的市场需求和流行趋势,实现纬编仿蕾丝织物设计,打造针织拼接蕾丝的产品,文章基于全自动电脑横机Stoll 530HP的编织工艺,以镂空花型编织装置(Stoll-devoréknit)开发了具有仿蕾丝效果的创意织片,完成由设计到成品生产的可操作化开发过程。从编织特性、工艺原理、纱线选择、花型设计及外观形态进行分析,将编织工艺与织物设计完美结合,为纬编针织服装产品的开发提供了一定的创新设计思路,同时也提升了产品的商业价值及市场竞争力。相较于传统型的针织拼接蕾丝面料的缝制过程,此设计思路于生产企业而言,缩短了产品制作周期,减少了额外的人工成本;于消费者而言,不透明区域与透明区域的无拼接缝份过渡,可给予消费者更好的穿着体验和舒适度。

摘要：从涡轮结构形式的角度探究了油气涡轮轴向力平衡问题。建立了半开式、开式与闭式3种局部进气裂解油气向心涡轮,通过数值仿真对比分析了设计工况下3种油气涡轮的气动性能与轴向力,并归纳总结了非设计工况下总轴向力随压比的变化规律。仿真结果表明:半开式、开式与闭式油气涡轮的总体气动性能相近但轴向力表现有明显的差别。当涡轮压比发生变化时,开式油气涡轮轴向力稳定性最好,半开式油气涡轮轴向力稳定性最差,闭式油气涡轮轴向力始终是3种油气涡轮中最小的。由结果分析可知,当涡轮压比低于3时,应避免选用半开式油气涡轮,而涡轮压比变化较大时,则宜采用开式油气涡轮,此外,在采用闭式油气涡轮时需要轴承预留足够的轴向载荷裕度。

摘要：针对无人机自主避障与目标追踪问题,以深度Q网络(DQN)算法为基础,提出一种多经验池深度Q网络(MP-DQN)算法,使无人机避障与追踪的成功率和算法的收敛性得到优化。更进一步,赋予无人机环境感知能力,并在奖励函数中设计了方向奖惩函数,提升了无人机对环境的泛化能力以及算法的整体性能。仿真结果表明,相较于DQN和双重DQN(DDQN)算法,MP-DQN算法具有更快的收敛速度、更短的追踪路径和更强的环境适应性。

摘要：为进一步提高骨修复材料的骨诱导性能,引入了BaTiO_3压电涂层。首先,通过等离子喷涂法在Ti基体上制备羟基磷灰石(HA)、Ti-HA和Ti-HA-BaTiO_3这3种生物涂层;然后,采用正交试验设计优化了喷涂工艺参数,用SEM/EDS对涂层的形貌和成分进行了表征,并通过划痕试验测试了涂层与基体的结合强度;最后,进行了细胞培养试验,用CCK-8法对细胞毒性进行了评价,并在SEM下观察了细胞的粘附形态。结果显示:细胞带有伪足,呈梭形和不规则多边形,且粘附在Ti-HA-BaTiO_3复合涂层表面;细胞伸展形态良好,涂层的细胞毒性等级不高于1级。可见,Ti-HA-BaTiO_3复合材料可以作为临床植入材料应用。

摘要：本文针对2016年6月山西、山东地区一次强对流活动,通过GRAPES(Global/Regional Assimilation and PredictionEnhancedSystem)云分析系统融合了多普勒雷达反射率三维组网拼图资料和ADTD(ActiveDirectory Topology Diagrammer)闪电定位资料,对模式初始场的云水、云冰等云微物理变量进行了调整和分析,并对这次强对流过程设计了3组数值试验。结果表明:(1)云分析系统在加入雷达反射率资料以后,能在模式初始场中较准确的计算模式的初始水物质;(2)闪电定位资料转换成的替代雷达反射率对原有的雷达反射率有一定的补充作用,使模式的初始场与真实状况更接近;(3)从模式降水的角度看,在加入雷达资料以后,GRAPES云分析可以显著提高6小时以内降水的模拟效果,而闪电定位资料的加入,对中雨以上量级的降水模拟有进一步的改进作用。

摘要：采用数值模拟的方法,对波形隔板结构复合通道的换热和流阻特性进行研究.设计了6种不同穿流孔孔径的隔板,研究孔径对通道中流动和换热的影响.将大小相间孔隔板结构的数值结果与已有实验结果进行对比,趋势符合较好.数值研究结果表明:在均孔隔板结构中,当孔径小时,通道换热好,同时流阻大;当孔径增大时,通道换热变差,同时流阻降低.当隔板上穿流孔总穿流面积一定时,大小相间孔的隔板结构与均孔隔板结构相比,换热略好些.

摘要：针对航空发动机压气机盘腔中流动与换热现象,采用该实验的方法对等温轴向通流旋转盘腔进行研究。通过对比不同工况下局部努塞尔数和平均努塞尔数的变化情况分析旋转腔中各力对流动与换热的影响,并总结努塞尔数与各无变量参数的经验公式。结果表明:盘腔内流动与换热主要由哥氏力、惯性力与离心力控制。腔内流动区域可划分为低半径位置惯性力占主导地位的惯性对流区与高半径位置哥氏力占主导地位的旋转对流区。轴向通流流量增大使惯性力增大,转速增高使哥氏力增大。惯性力与哥氏力的增加都会增强换热,两个力对彼此对换热的影响有削弱作用,两个力的综合作用使不同工况中不同半径位置的换热变化情况不同。平均努塞尔数与局部努塞尔数随变量的变化情况基本一致。