柔性低温多晶硅薄膜晶体管的弯曲稳定性

研究了以聚酰亚胺为基板的p型低温多晶硅薄膜晶体管在不同弯曲半径下的偏压稳定性。当曲率半径从15 mm变到3 mm时,在拉伸弯曲状态下,阈值电压和平坦时保持一致(Vth=-1.34 V),迁移率μsat从45.65 cm~2/(V·s)降到45.17 cm~2/(V·s),开关比增大;在压缩弯曲状态下,转移特性曲线和平坦状态保持了非常好的一致性。在最小弯曲半径为3 mm时,进行了正负偏压稳定性测试,结果表明,器件依然具有很好的稳定性。     

修正的Kadomtsev-Petviasvili方程的对称和守恒律

修正Kadomtsev-Petviasvili (MKP)方程是非线性偏微分方程和物理学中的一个重要模型. 最近楼森岳教授指出从可积系统的一个点李对称出发, 可以得到无穷多的守恒律. 应用楼教授的思想, 首先研究MKP方程的经典的李点对称, 然后根据二阶延拓结构(Lie-Bäcklund算子), 构造MKP方程的无穷多守恒律.     

227-W output all-fiberized Tm-doped fiber laser at 1908 nm

In this paper, we report that a diode-pumped thulium-doped double clad silica fiber laser can provide powers of up to 227 W at 1908 nm, corresponding to a slope efficiency of 54.3%, and an optical-to-optical efficiency of 51.2%. The output power, to the best of our knowledge, is the highest output at 1908 nm. The beam quality M2 factor is about 1.56. Also discussed in this paper is the dependence of the laser performance on fiber length.     

Effect of noncircular orifice plates on the near flow field of turbulent free jets

In this paper, we experimentally investigate the near-field flow characteristics of turbulent free jets respectively issued from circular, triangular, diamond, rectangular, and notched-rectangular orifice plates into air surroundings. All the orifice plates have identical opening areas or equivalent diameters（De） and their aspect ratios（AR） range from 1 to 6.5. Planar particle image velocimetry（PIV） is used to measure the velocity field at the same Reynolds number of Re = 5 × 10^4,where Re = Ue De/ν with Ue being the exit bulk velocity and ν the kinematic viscosity of fluid. The mean and turbulent velocity fields of all the five jets are compared in detail. Results show that the noncircular jets can enhance the entrainment rate, reflected by the higher acceleration rates of mean velocity decay and spread, shorten the length of the unmixed core,expedite the increase of turbulent intensity compared with the circular counterpart shortened unmixed core, and increase turbulent intensity comparing to the circular counterpart. Among the five jets, the rectangular jet（AR = 6.5） produces the greatest decay rate of the near-field mean velocity, postpones the position at which the 鈥榓xis-switching鈥檖henomenon occurs. This supports that axis switching phenomenon strongly depends on jet initial conditions. In addition, the hump in the centerline variation of the turbulence intensity is observed in the rectangular and triangular jets, but not in the circular jet, nor in diamond jet nor in notched-rectangular jet.     

Dressed Dark Solitons of the Defocusing Nonlinear Schrodinger Equation

The nonlinear Schrodinger equation is proved to be consistent-tanh-expansion （CTE） solvable. Some types of dark soliton solutions dressed by cnoidal periodic waves are obtained by means of the CTE method.     

Interactions between Solitons and Cnoidal Periodic Waves of the Gardner Equation

The Gardner equation is one of the most important prototypic models in nonlinear physics. Many scholars pay much attention to the Gardner equation and various nonlinear excitations of the Gardner equation have been found by many methods. However, it is very difficult to find interaction solutions among different types of nonlinear excitations. In this work, with the help of the Riccati equation, the Gardner equation is solved by the consistent Riccati expansion. Furthermore, we obtain the soliton-cnoidal wave interaction solutions of the Gardner equation.     

电流与磁场互生关系的假想与应用

在电流与磁场互生及相互作用关系判断上,目前有安培定则、左手定则、右手定则,但对于电流与磁场互生及相互作用的内在机理却没有探讨。本文从微观假想电子磁场及其特性,通过假想解释了电子、电流、磁场及其相互作用的内在机理。通过内在机理解释了电流与磁场的安培定则、左手定则、右手定则等不同的外在表现形式,并通过内在机理的假想推导出电流与磁场存在的某些特性,以供深一步的研究和探索。     

用清除羟自由基法评价竹叶提取物抗氧化能力

进行了Fe2+与邻二氮菲生成红色配合物的吸收光谱,抗氧化剂TBHQ及竹叶提取物样品对清除羟自由基能力的研究。分光光度法测定抗氧化剂清除羟自由基能力的测定波长为509.1 nm。以IC₅₀值(清除率为50%时,抗氧化剂的浓度值)作为评价抗氧化剂清除羟自由基能力的指标,测得合成抗氧化剂和效果最好竹叶提取物样品IC₅₀值分别为0.040(TBHQ),0.378(M20),0.323(M40),0.334(M60),M20, M40, M60等竹叶提取物可以作为天然抗氧化剂进行开发。     

基于ALE方法的飞机水面降落过程

为了研究飞机水面降落过程中的动态响应规律,采用arbitrary Lagrangian-Eulerian(ALE)方法开展了飞机水面降落的动力学分析。研究了飞机水面降落过程的速度变化规律,结果表明,降落速度和飞行速度在飞机入水的初始阶段变化较快,随后变化幅度趋于平缓。分析了不同降落速度、飞行速度和降落仰角下的机身结构响应,得到了飞机水面降落时结构响应随时间的变化规律。机身结构应力在入水的初始阶段达到最大值,随后迅速下降,最后保持稳定。飞机结构的最大变形也出现在入水的初始阶段,随后迅速回复到初始状态。对比了降落速度、飞行速度和降落仰角对飞机结构响应的影响程度,结果表明降落速度对结构响应的影响程度最大,降落仰角次之,飞行速度的影响最小。 更多还原