RUPTURE OF THIN METAL TUBES BY NORMAL AND OBLIQUE IMPACT OF BLUNT CONICALNOSED MISSILES: EXPERIMENTS

Impact tests at both normal and oblique angles of incidence were conducted on thin mild tubes using a moderate size of 90° conical-nosed missiles. The minimum impact speed that generated cracks through the thickness of the wall, termed the speed for rupture, was measured, and various modes of rupture were identified. For a thin tube hit by a missile at a normal angle of obliquity at the speed for rupture, the contact region spreads across the nose of the missile, and the transverse shear deformation is predominant in the final failure process. If the angle of obliquity is 30°, the missile pierces a hole through the wall of the tube. At the speed for rupture, the kinetic energy of the missile for oblique angle 30° is only about 45% that required for plugging at a normal angle of obliquity. The project sponsored by National Natural Science Foundation of China(No. 19842001, 19872048) and Scientific Research Foundation for Returned Overseas Chinese Scholars of State Education Commission and Shanxi Province of China.     

Elliptic Curves and Three-Dimensional Flow Patterns

This paper is concerned with the geometry of flow patterns inthe classical problem of an impulsely-started, incompressible,axisymmetric, laminar jet generated by a point force. The second andthird invariants of the velocity gradient tensor, evaluated at criticalpoints in the jet, describe the fundamental dependence of the flow onthe jet Reynolds number. As the Reynolds number is increased from zeroto infinity, the critical points follow elliptic curves in the space ofinvariants and rational roots occur at bifurcation points in this space.The corresponding invariants of the acceleration gradient tensor traceout a trajectory with infinitely many, densely spaced rational roots.The results provide new insight into the viscous and pressure forceswhich act in the jet and the balance between strain and rotation whichleads to the onset of a starting vortex.     

电雾化装置及雾化模型研究

本文介绍了新研制的电雾化实验装置及其测试系统。一系列实验表明该系统运行可靠。在该装置上进行的实验表明,电雾化现象与溶液电导率、介电常数、表面张力、粘性以及电压、流量有关。电雾化现象中存在“滴”模型、“脉动”模型、“锥－射流”模型、“不稳定”模型等几种不同的流动状态。而在“锥－射流”模型时,溶液具有单分散的尺度分布。本文还介绍了酒精溶液在民雾化过程中出现“锥－射流”现象的区域。     

含悬浮固粒射流界面稳定性研究

利用气固两相耦合模型,理论推导出含悬浮固粒射流的稳定性方程,通过数值计算得到了两相射流稳定性特征曲线、固气扰动速度比值幅值曲线及固气相位差曲线,进而得到了关于固粒对流场中扰动增长和传播的影响及失稳过程中固粒扰动特性的结论。这些结论对于两相射流发展的认识和工程实际中实施对两相射流场的人工控制有重要意义。     

熔喷双槽形喷嘴气体射流流场初探

在熔喷非织造布加工中,气体射流作为工作介质使聚合物熔体实现拉伸,气体射流流场的研究对熔喷气流拉抻数学模型研究非常重要。熔喷双槽形喷嘴形成的流场可以看作两股平面射流的合成。从单个点涡的性质出发,研究了涡偶的性质和涡偶代替射流的可行性。研究表明,在喷丝孔轴线附近,涡偶和射流的速度分布趋势相同,且有比较相近的速度分布,从而说明以涡偶代替射流是可行的。在此基础上,用两个涡偶分别代替两股射流,然后进行合成,推导出两股射流合成后速度分布的理论公式,该公式的计算结果与实验结果吻合较好。将该公式引入熔喷气流拉伸数学模型,预测出的纤维直径与采用经验公式时的预测结果几乎完全相同。结果表明,应用涡偶代替射流推导出的气流速度分布公式能够较好地描述熔喷双槽形喷嘴气体射流流场,可以用于完善熔喷气流拉伸数学模型。     

欠膨胀高速射流的压力均一化过程

发展了分析欠膨胀高速湍流射流近场特性的数值,计算了不同背压比条件下声速喷管出口附近膨胀区的激波胞格结构,揭示了压力一化过程的的机制。     

电场作用下导电射流稳定性的理论与实验研究

建立导电射流在径向电场作用下的线性稳定性粘性模型,通过正则模方法,推导了轴对称和非轴对称模态下的色散关系,通过计算求得增长率随波数及电欧拉数的变化,并在理论上预测了最有可能波长.选用酒精和酒精甘油混合物作实验液体,观察了径向电场对射流不稳定性行为的影响规律,并测量射流表面波的波长.实验结果和理论结果在定性方面取得了较好的一致.但通过与实验比较,理论预测的最有可能波长在非轴对称模态出现较大偏差,普遍比实验结果小.而且,实验表明,最大增长率并不是判断主导模态的好标准,因为在非轴对称的最大增长率小于轴对称的最大增长率情况下,实验显示非轴对称模态要比轴对称模态明显了.因此,对于非轴对称的不稳定机理,需要进一步研究.对轴对称模态,理论给出了较好的预测.     

大直径射流的放电特性及其等离子体参数和活性粒子分布的光谱诊断

大气压等离子体射流因其产生的等离子体羽富含活性粒子而在废水净化、元素探测、材料处理等方面具有良好的应用前景.通常等离子体羽的直径较小,限制了其工作效率.针对于此,利用交流电压激励大气压氩气等离子体射流,产生了直径约为14 m m的大尺度均匀等离子体羽.采用发射光谱法对电子密度和氧原子浓度随不同实验参数的变化关系进行了研...     

层流氩等离子体射流温度的测量

 采用给水冷管状静电探针施加负偏置电压、并使探针以一定速度垂直于射流轴线扫过层流氩等离子体射流的方法,测量探针所收集到的累积离子饱和电流随侧向位置的变化,利用Abel变换推导出了局部离子饱和电流密度沿射流径向的分布;采用自制的水冷动压探针,以动态扫描法测量了射流动压沿射流径向的分布;根据局部离子饱和电流密度和射流动压的测量数据,由理论关系式推导出了等离子体射流横截面上的温度分布,同时,采用谱线相对强度法测量了等离子体射流的激发温度。结果表明：两种方法得到的等离子体射流中心温度吻合较好,所得到的射流中心温度随弧电流加大而增大的变化趋势也一致。     

Large eddy simulation of incompressible free round jet with discontinuous Galerkin method

In the paper, discontinuous Galerkin method is applied to simulation of incompressible free round turbulent jet using large eddy simulation with eddy viscosity approach. The solution algorithm is based on the classical projection method, but instead of the solution of the Poisson equation, a parabolic equation is advanced in pseudo‐time, which provides the pressure field ensuring the proper pressure–velocity coupling. For time and pseudo‐time integration, explicit Runge–Kutta method is employed. The computational meshes consist of hexahedral elements with flat faces. Within a given finite element, all flow variables are expressed with modal expansions of the same order (including velocity and pressure). Discretisation of the viscous terms in the Navier–Stokes equations and Laplacian in the Poisson equation is stabilised with mixed finite element approach. The correctness of the solution algorithm is verified in a commonly used test case of laminar flow in 3D lid‐driven cavity. The results of computations of the free jet are compared with experimental and numerical reference data, the latter obtained from the high‐order pseudospectral code. The statistics of centerline flow velocity – mean velocity and its fluctuations – show satisfactory agreement with the reference data. Copyright © 2015 John Wiley & Sons, Ltd.