Effect of moisture content on conveying characteristics of pulverized coal for pressurized entrained flow gasification

During the pneumatic conveying, pulverized coal with different moisture contents may develop substantial difference in flow characteristics, whose cause is not fully understood. This study focused on influence of moisture content on conveying characteristics in an experimental test facility with the conveying pressure up to 4 MPa. The experiments included soft coal and lignite with similar density and particle size. With the increase in moisture content, the mass flow rate decreased for lignite (3.24% < M < 8.18%) but increased at first and then decreased for soft coal (0.4% < M < 6.18%) at same operating parameters. The flowability of soft coal was worse than that of lignite at similar operating parameters and external moisture content. The extremal conveying moisture contents of two coal types were obtained. The particle charge and surface moisture content were investigated to indicate influence mechanism of moisture content on mass flow rate in pneumatic conveying at high pressure. Pressure drop of soft coal was greater than that of lignite for same test section. The conveying phase diagram of dense-phase pulverized coal at high pressure was obtained and the pressure drops through different test sections were compared and analyzed. The bend loss factor rose with the increase in moisture content and was independent of conveying velocity and solid-gas ratio in dense-phase pneumatic conveying at high pressure.     

Numerical investigation of the effects of structural geometric and material nonlinearities on limit-cycle oscillation of a cropped delta wing

This article presents numerical simulations of the limit-cycle oscillation (LCO) of a cropped delta wing in order to investigate the effects of structural geometric and material nonlinearities on aeroelastic behavior. In the computational model, the structural part included both the geometric nonlinearity that arises from large deflections, and the material nonlinearity that originates from plasticity. The Euler equations were employed in the fluid part to describe the transonic aerodynamics. Moreover, the load transfer was conducted using a 3-D interpolating procedure, and the interfaces between the structural and aerodynamic domains were constructed in the form of an exact match. The flutter and LCO behaviors of the cropped delta wing were simulated using the coupling model, and the results were compared with existing experimental measurements. For lower dynamic pressures, the geometric nonlinearity provided the proper mechanism for the development of the LCO, and the numerical results correlated with the experimental values. For higher dynamic pressures, the material nonlinearity led to a rapid rise in the LCO amplitude, and the simulated varying trend was consistent with the experimental observation. This study demonstrated that the LCO of the cropped delta wing was not only closely related to geometric nonlinearity, but was also remarkably affected by material nonlinearity.     

Confined impinging twin air jets at high Reynolds numbers

An experimental study is carried out to investigate flow characteristics of confined twin jets issuing from the lower surface and impinging normally on the upper surface. Pressure distributions on the impingement and confinement plates were obtained for Reynolds numbers ranging from 30,000 to 50,000, nozzle-to-plate spacing (H/D) in the range of 0.5-4 and jet-to-jet spacing (L/D) in the range of 0.5-2. Smoke-wire technique was used to visualize the flow behavior. The effects of Reynolds number, nozzle-to-plate spacing and jet-to-jet spacing on the flow structure are examined. The subatmospheric regions occur on both impingement and confinement plates at the nozzle-to-plate spacing up to 1 for all studied Reynolds numbers and jet-to-jet spacings in consideration. They lie nearly up to the same radial location at both surfaces and move radially outward from the stagnation points with increasing nozzle-to-plate spacing and jet-to-jet spacing. It is concluded that there exists a relation between the subatmospheric regions and peaks in heat transfer coefficients for low spacings in the impinging jets.     

抗阵风载荷的小型无人飞行器设计及相关风洞舵效比较

本文目的在于探索验证微小型飞行器的气动布局与抗突风载荷能力的关系,结合风洞试验验证了结果并进行了数据分析。在低雷诺数条件下采用大边条、小展弦比非常规的气动布局设计,根据性能指标要求对飞行器的机翼面积、翼展、翼型等相关参数进行了分析设计;运用数值模拟等手段对全机简化模型进行了气动力计算,对结果进了行初步的定性分析,为初始的设计提供了验证;结合实际的靶机制作得到了实际飞机的风洞验证缩比模型,对其进行了风洞的常规测力实验。根据风洞试验结果对飞机升降舵舵面与副翼舵面偏转0°、±15°、±30°的气动性能进行了评估,为进一步的理论分析提供依据。结合实际外场飞行实验情况得出飞行器的实际气动性能,并对大量相关风洞试验数据进行了分析;探索性地给出了一条适用于微小型飞行器进行的新设计方法和设计流程,为设计适应于阵风载荷等恶劣气候条件下微小的型飞行器提供了参考新思路。     

盐岩流变特性及盐腔长期稳定性研究进展

介绍了地下盐腔长期运营过程中盐腔收敛变形和有效容积丧失等问题, 从盐岩流变实验研究、盐岩流变本构关系建模、盐腔长期稳定评价等方面综述了盐岩流变学研究进展. 文章指出, 将盐岩流变本构模型与流变过程中盐岩微细观尺度上的损伤演化物理机制相融合, 是盐岩流变学一个值得关注的研究方向.     

钝体绕流的分隔板控制技术研究进展

钝体是工程中一种常见结构,流体绕过钝体时产生的旋涡脱落易诱发结构振动,进而导致结构破坏．钝体后安装分隔板是一种典型的被动控制技术,分隔板推迟钝体尾流区剪切层之间的相互作用,进而有效改变钝体后旋涡脱落及尾迹特性,延长结构寿命,并且可以利用钝体一分隔板结构进行能量收集．本文全面回顾了利用分隔板进行流动控制和能量收集的研究及...     

气体钻水平井井径扩大环空流动特征的数值模拟

由于气体钻水平井中岩屑受力状态与直井有很大不同,特另0是遇到井径扩大,更是携岩的关键点。因此,在分析了气体钻水平并岩屑运移特点以及建立环空连续性方程和动能方程的基础上,以实际并为例考虑了不同井径扩大率,数值模拟了其扩径段气固两相的流动状态,包括气固速度、岩屑浓度、压力分布等。研究结果表明：气体在经历扩径段时环空压力有个降落又回升的过程,随着井眼扩径系数的增大,压力下降又回升,所经历的长度会逐渐增长;扩径系数大于一定值时,扩径变径处存在一定区域的零流动区;扩径系数越大,低速区和回流区就越大越长,扩径下部区域越容易堆积岩屑,填充井眼。     

土体水分传输的温度效应试验系统设计与应用

自制了一套用于研究温度作用下土体水分传输机制的室内试验模拟系统.采用水浴加热替代电阻丝直接加热的方案,解决加热不均匀且不容易控制温度的难题.应用串行通讯接口技术把智能温度控制仪表和微机连接,实现了温度自动控制和采集的自动化.开展了7组试验耗时接近1年,试验结果表明,该系统性能稳定、部件之间兼容性较好,连续工作30天温度...     

大变形柔性多体系统非线性动力学数值仿真与实验研究

提出了一种作大范围运动柔性梁的非接触动态测试技术.在基于位移的柔性多体系统几何精确建模及非线性有限元分析技术的基础上,利用EAGLE-500运动分析系统及其相应的分析软件对作大范围运动钛合金柔性梁作了实验研究,并且利用之前提出的几何精确梁理论进行数值仿真.数值仿真结果与实验结果完全吻合,验证了作者所提的几何精确梁理论及...     

正交约束下的D-最优试验设计

针对一类因素间具有正交约束的回归模型的试验设计问题,以D-最优为准则,以加速度计试验设计为背景,从试验点的均衡分布原则出发,以不同试验环境下合加速度大小为依据,给出了不同环境下球内接正多面体的试验方法,通过进一步计算和深入分析表明,单球面时为避免信息矩阵降秩应采用不同安装方式,降低模型维数以达到试验目的;两球面下试验设计的优劣与两个半径的大小有关,半径越大计划越优,而且信息矩阵的秩最大时两个球半径之间呈近似线性关系.试验结果的优劣还受到初始安装位置的影响,为了达到最优化,应使合加速度方向与加速度计的某个轴同向.