低速轴对称层流射流流动形态和失稳机制的实验研究

本文应用染色液和悬浮粒子显示方法,进一步实验研究轴对称层流射流的流动形态及其失稳机制。首次成功地在从一定口径的喷嘴流出的低速轴对称层流射流中观察到环形回流流动。给出了射流随速度演化及实验容器边界对其流动形态影响的显示照片,发现实际射流的轴对称波动及失稳过程正好对应射流在容器底部产生的环形旋涡的生长和破碎过程。本文认为由于实验空间有限尺度对流动的限制改变了原来射流的流动形态和流场空间的拓扑性质,射流与实际边界的相互作用对实际射流的失稳和转捩有重要的影响。     

用PSM模型模拟聚合物熔体轴对称收缩流动

采用模拟黏弹流体挤出胀大的方法，计算了IUPAC-LDPE熔体经过4：1轴对称收缩流道的流动．计算的相对涡强度、入口校正和献中的结果基本一致，给出的流场也显示出计算结果是合理的．表明该方法能够适用于用积分型PSM模型表征的黏弹流体在收缩流道内的流动模拟．     

高压旋转射流流动特性的实验研究

测量了叶轮导引高压射流喷嘴在不同叶轮螺旋倾角和喷嘴收缩角下高压水的喷射形状参数,通过分析给陋了此种射流的外边界曲线方程形式及射流扩散角与叶轮螺旋倾角、喷嘴收缩角的关系,最后对射流机理进行了探讨,并给出一种微团轨道模型研究方法。     

扭矩转化器（T／C）内部叶片流道流场的二维PIV实验研究

本文利用二维ＰＩＶ技术研究了汽车无级调连装置中扭矩转化器内部叶片流道流场的复杂流动,实验结果表明泵和透平在不同转速下,静子叶片流道中的流场体现出不同的流动特征,文中还对实验误差进行了分析,提出了减少误差的措施,通过叶栅流动理论分析说明了本文结果的可靠性。     

零重力条件下低温射流抑制大尺寸液氢储罐热分层的数值研究

液氢是一种常用的沸点低、易蒸发的空间低温推进剂. 空间微重力环境中浮力对流被极大减弱,当推进剂储罐壁面存在局部漏热时,储罐内部气液两相流体系会出现环绕漏热源的热分层现象,引起局部过热沸腾,导致储罐内部压力急剧增大,危害系统结构安全. 利用低温射流抑制储罐热分层现象是一种有效手段. 低温流体通过设置在储罐内部的射流喷嘴与储罐内部的流体混合,消减局部高温,实现温度的均匀化. 采用全充满的二维大尺寸储罐模型,对零重力条件下液氢储罐内局部漏热引起的热分层现象开展了数值模拟,主要分析了位于靠近储罐底部的漏热带以及出口衔接段漏热带漏热形成的局部热分层现象的抑制和消除,并研究了不同低温射流条件对于消除零重力条件下液氢储罐内部热分层效果的影响. 研究结果表明对于大尺寸储罐,当采用圆形射流喷嘴且低温射流条件相同时,射流喷嘴的位置对罐体内部热分层消除效果影响不是很明显. 当射流喷嘴位于储罐内部同一相对位置且入射流量相同时,圆形射流喷嘴因出流方向更集中,罐内流场演变更快,消除热分层比半球形射流喷嘴更有效.      

颗粒在黏弹性流体扩张和收缩流中沉降的格子Boltzmann模拟分析

对于Oldroyd-B型黏弹性流体，本文应用格子Boltzmann方法(LBM)，实现了流体在二维1:3扩张流道及3:1收缩流道中流动的数值模拟，获得了黏弹性流体在扩张和收缩流道中的流场分布．结合颗粒的受力和运动规则，基于点源颗粒模型，数值分析了颗粒在扩张流和收缩流中的沉降过程和特征，讨论了颗粒相对质量和起始位置以及雷诺数Re和威森伯格数Wi对颗粒沉降特征的影响．结果表明，颗粒相对质量和起始位置以及Re对颗粒沉降轨迹和落点影响较大，而Wi的影响则较小．     

小口径轴对称收缩喷嘴射流冲击大平板噪声指向特性研究

实验研究了3毫米口径轴对称收缩喷嘴在各种压比下射流垂直冲击和倾斜冲击坚固大平板产生的噪声的指向特性。发现噪声在过平板法线和喷嘴轴线的平面内呈近似四瓣分布，当喷嘴与平板距离减小时，指向壁射流下游的瓣得到增强，反之，指向喷嘴上游的瓣得到增强。喷嘴压比增加时，指向壁射流下游的瓣得到增强，反之，指向喷嘴上游的瓣得到增强。根据自由射流噪声的基本指向特性、射流冲击噪声基本指向特性、声波在平板处发生镜面反射和声波能量叠加的设定，建立了一个冲击射流总体噪声指向特性的模型，成功解释了实验结果，并揭示了形成冲击射流总体噪声指向特性的内在机理。     

非线性强弱对轴对称射流拟序结构影响的研究

本文采用三维离散涡方法对轴对称不可压射流进行了数值模拟。由于Re数的大小体现出流场方程中非线性项的相对强弱,所以文中研究了不同Re数对射流中拟序结构的影响。文中提出并运用了一种有效的涡增加技术以提高涡方法的分辨率和精度,描绘了射流中展向涡的空间和时间发展,细致研究了涡的卷起、配对与合并现象。结果说明,在高Re数即非线性项相对较大的范围内,轴对称射流的发展主要受大尺度拟序结构的支配,而粘性则抑制大涡的产生与发展;Re数越大,非线性越强,同一时刻流场中大涡的数量越多,发展越充分。计算结果和实验一致,对实际射流的控制有重要意义。     

分离再附流动的实验研究

综述了二维前后向台阶,T型结构以及轴对称纯体等典型几何结构的分离再附流动的实验研究．介绍了不同模型分离再附流场特性以及它们之间的异同．详细论述了流动各参数对流场的影响,并简要分析了分离再附流动中存在的问题和发展方向．      

不定原点喷嘴射流中流体物理的实验研究(英文)

为了能够更好地了解不定源喷嘴(indeterminate origin nozzle)射流中的物理过程,本文应用平面激光诱导荧光技术对一个大尺度的水射流进行了实验研究。流场显示的实验结果表明不定源喷嘴在射流的剪切层引入了蘑菇形反向旋转的涡对。这些涡的矢量方向与射流方向相同或相反,被称为流向涡(streamwise vortex)。由于射流中存在开尔文-亥姆霍兹不稳定,每当一个横向涡(spanwise vortex,即涡的矢量方向与射流方向垂直)从喷嘴脱流时会产生瞬时的低压,该瞬时低压促使向内发展的流向涡对在喷嘴的凹槽处生成。这些涡对在向下游流动的过程中会重组并在喷嘴的尖峰面生成向外发展的涡对。这些流向涡极大地影响了射流的发展。流向涡与横向涡的相互作用促使射流更早地发展成为湍流。由于流向涡同时也在射流中引入了径向的剪切流动,因此导致了更多的湍流生成从而增强了射流与周围流体的混合。     

大学物理《力学》中的自由度分析

对《力学》中的物体自由度进行多方面分析,以深化教学、提高学生正 确分析物理问题的能力.使用实际教学分析的研究方法,在《力学》范围内讨论自由度与坐标、 自由与约束的关系并得以下结论: (1) 同一物体的自由度随其所在的``空间'不同而不同, 不因坐标系的选取不同而 异, 在同类参考系中不因参考系的动静而有别;(2)自由度遵循叠加原理. 讨论了质点系的总自由度及相关计算问题,并指出研究《力学》中自由度的意义.     

Development and design of new methods of measurement of state of strain of structures

The present paper deals with development and design of new methods utilizing Wiedemann's effect for determination of state of strain in building structures. Wiedemann's effect and some features of torsional strain of magnetic field are the basis of new experimental method. Especially the point electromagnetic strain gages using the effect of pure torsion of electromagnetic field to enable universal examination. For strain-gage measurements, almost all physical quantities are used which can be related to the variation in length of the structures. From the electric strain measurements, the most commonly used methods are the measurements by resonance-wire strain gages or by electric-resistance strain gages. In this paper, electromagnetic strain gages are discussed using the Wiedemann effect, and the author describes some new measuring equipment and his own suggestions and methods based on an application of this effect.     

Calculation of aerodynamic characteristics of arrays of profiles of arbitrary shape

It is well known that the problem on nonseparating potential flow of an incompressible fluid about an array of profiles reduces to an integral equation for a certain real function, determined on the contours of the profiles of the array. As such a function one can take, as was done, for instance, in [1–5], the relative velocity of the fluid on the profiles of the array. For arrays of profiles of arbitrary shape it is necessary to solve the corresponding integral equation numerically. In the particular examples of the calculation of aerodynamic arrays that are available [1–3] the numerical methods used were based on the approximate evaluation of contour integrals by rectangle formulas. As investigations showed, sizeable errors arose thereby in the approximate solution obtained, these being especially significant in the case of curved profiles of relatively small bulk. In the present paper a method for the numerical solution of the integral equation obtained in [5] is proposed. The method is based on the replacement of a profile of the array with an inscribed N polygon, the length of whose sides is of the order N^–1 and whose internal angles are close to . Convergence with increasing N of the numerical solution to an exact solution of the integral equations at the reference points is demonstrated. Examples of the calculation are given.Novosibirsk. Translated from Izvestiya Akademii Nauk SSSR. Mekhanika Zhidkosti i Gaza, No. 2, pp. 105–112, March–April, 1972.     

Method of constructing estimates of the solution of equations of filtration of an aerated liquid

The exact solutions of the nonlinear equations of filtration of an aerated liquid have been obtained in [1–3]. In [4] the system of equations of an aerated liquid have been reduced to the heat-conduction equation under certain assumptions. An approximate method of computing the nonsteady flow of an aerated liquid is given in [5], where the real flow pattern is replaced by a computational scheme of successive change of stationary states. In [6] the same problem is solved by the method of averaging. In the present article estimates of the solution of the equations for nonstationary filtration of an aerated liquid in one-dimensional layer are constructed under certain conditions imposed on the desired functions. These estimates can be used as approximate solutions with known error or for the verification of the accuracy of different approximate methods. We note that the use of comparison theorem for the estimate of solutions of equations of nonlinear filtration is discussed in [7–9]. The methods of constructing estimates of solutions of various problems of heat conduction are given in [10, 11]