首页 | 本学科首页   官方微博 | 高级检索  
相似文献
 共查询到19条相似文献,搜索用时 93 毫秒
1.
界面曲率对空化的演变及结构载荷的影响   总被引:1,自引:0,他引:1  
研究了近体水下爆炸中结构表面外形的变化对空化的形成、演变及结构载荷的影响.为了真实地考虑流体与固体的非线性相互作用,近期发展的流-固耦合多介质Riemann问题技术和修正的虚拟介质方法被推广应用于处理流体与固体的相互作用中.研究发现,凹的表面设计不但可以导致爆炸冲击波局部汇聚和强化,而且随后可以强化空化破裂所造成的冲击,研究进一步发现,这种强化作用还是非线性的,随曲率的增加而非线性增强;相反地,凸的表面设计可以减低爆炸冲击波冲击,而且可以弱化空化的产生,但其影响是非常有限的.  相似文献   

2.
王革  张斌 《计算力学学报》2009,26(3):442-445
原始的虚拟流方法(GFM)在计算强激波和物质界面作用时无法得到正确的计算结果,而改进虚拟流方法(MGFM)处理这类问题的能力大大提高.本文用Level set捕获物质界面,用MGFM方法定义虚拟流节点参数,Euler方程采用HLLC格式离散求解,完成了强激波和物质界面作用的一维和二维数值实验.结果表明改进虚拟流方法在强激波与物质界面作用中的应用是成功的.  相似文献   

3.
利用Level Set方法隐式捕捉界面并能处理复杂的物质界面及其拓扑结构变化(如合并、交叉、破碎等)情况的优势,基于可压缩N-S方程的预处理技术,采用基于界面两侧介质黎曼关系的修正虚拟流体方法对介质边界进行处理;将只能应用于可压缩流动界面模拟的修正虚拟流体方法推广应用于不可压缩流动问题的模拟,数值模拟了气-水运动界面与近水面飞行器的相互影响规律。通过与将水面视为对称面的简化模型对比发现:利用自由运动界面模型计算的NACA6409翼型升力较小,能更准确地反映飞行器流场对水面形状的影响,其结果更为符合实际;文中还对比了翼型距水面不同高度时的结果,得到了翼型受水面影响的强弱与翼型距水面的高度成反比的结论。  相似文献   

4.
本文采用边界元法研究水与粘弹性介质在地震波入射条件下的相互作用问题。首先,采用半空间格林函数建立液体介质区域的边界元方程,然后考虑液—固界面的连续条件,获得水对固体介质的影响矩阵,最后用此影响矩阵修正固体介质的边界元方程。通过对简单问题的计算表明,采用本文方法求解流—固相互作用问题,其计算量与单独求解固体介质的波动问题时相当。  相似文献   

5.
为了克服原始虚拟流方法(ghost fluid method,GFM)在处理激波与大密度比流体-流体(气-水)界面相互作用时遇到的困难,采用真实虚拟流法(real ghost fluid method,RGFM)处理流体界面附近的虚拟点,结合HLLC(Harten-Lax-Van Leer with contact discontinuities)格式求解Euler方程,采用五阶WENO(weighted essentially nonoscillatory)格式求解level set输运方程。通过一维和二维算例的物质界面捕捉研究,证明RGFM在处理小密度比界面问题时优于GFM,同时RGFM还可用于求解激波与大密度比物质界面相互作用问题。计算表明,将RGFM引入到本文算法中,可精确捕捉到激波与界面(气-气、气-水界面)相互作用的变化细节,包括大密度比界面的剧烈变形和破碎,并具有较高的计算分辨率。  相似文献   

6.
两介质流界面-激波相互作用RKDG 方法应用分析   总被引:2,自引:2,他引:0  
冯峰  王强 《计算力学学报》2012,29(2):255-261
为精确模拟多介质流界面运动现象,采用RKDG方法结合虚拟流体方法对气-气、气-液和液-气等多种界面-激波相互作用问题展开研究。数值结果表明,RKDG方法的时空高精度特征使其能够精确、稳健地求解各种复杂界面运动问题。最后,对水下激波自由面折射问题用多种DG格式限制器进行了计算,对比了它们的间断捕捉能力。  相似文献   

7.
目前流体流动与传热问题的研究大都基于确定性工况条件, 而现实流体流动与传热问题中存在着大量不确定性因素, 计算流体力学的不确定性量化提供了一种理解流体物性、边界条件与初始条件等不确定性因素对模拟结果影响的能力. 为揭示随机多孔介质内顺磁性流体热磁对流的传播规律与演化特征, 本文发展了一种基于侵入式多项式混沌展开法的热磁对流不确定性量化数理模型与算法程序. 该方法分别利用Karhunen-Loeve展开与多项式混沌展开表达输入随机参数与输出响应量, 同时利用伽辽金投影方法将随机热磁对流控制方程解耦为一组可以应用有限元修正方法求解的确定性控制方程, 并对输出响应量多项式混沌进行求解, 最后采用随机投影法求解相应的确定性控制方程中的混沌系数, 得到输出响应量的统计特征与混沌效应. 热磁对流不确定性量化表明多孔介质孔隙率不确定性通过控制方程演化, 进而影响着多孔介质方腔内顺磁性流体热磁对流, 顺磁性流体热磁对流呈现出显著的混沌效应. 与蒙特卡罗法预测结果相比, 两者计算结果吻合良好, 但侵入式混沌多项式展开法计算量显著减少.   相似文献   

8.
应用弹性薄板的基本理论和流体力学的基本方程,采用相容拉格朗日-欧拉法,深入研究弹性薄板在理想流体横向绕流时的弯曲变形及应力状态.结合接触面处流体与弹性薄板相互作用的运动学方程和动力学方程,建立不间断横向绕流条件下弹性薄板弯曲变形的微分方程.根据边界条件给出挠度函数,采用泰勒展开的方法得到弹性薄板变形与应力的表达式.通过具体算例分析弹性体参数对变形以及应力大小的影响.其分析结果可为流体作用下弹性薄板的强度与刚度设计提供参考.  相似文献   

9.
将多相流领域内的虚拟区域法引入到流固耦合问题的分析中,将固体视为应变率为 零的虚拟流体,对流体和虚拟流体均以速度和压强作为基本变量,采用Navier-Stokes方 程作为控制方程,同时求解流体域和虚拟流体域, 得到整个计算域的流场分布,应用分布式拉 格朗日乘子法在虚拟流体域上施加刚体约束, 以保持虚拟流体的刚体外形和运动形式,最终建 立一种流固耦合模型及其数值求解方法. 通过对粒子流问题和流固耦合问题进行数值模拟, 验证了此模型的正确性和求解大变形/运动流固耦合问题的有效性.  相似文献   

10.
朱合华  陈庆 《力学学报》2017,49(1):41-47
有效介质方法是常用的细观力学方法之一.其可用于计算多相材料的有效性能,并建立材料微细观结构和宏观性能的定量关系;有助于指导新材料设计,减少试验工作量等.然而,当夹杂含量升高时,传统有效介质方法的计算精度下降.本文以两相材料为研究对象,提出一种新的参考介质,即:为更合理考虑不同夹杂颗粒间的相互作用,假定参考介质的应变是基体相平均应变和某一修正张量的双点积.在此基础上,推导了新参考介质下两相材料的有效模量表达式,并给出该修正张量的近似计算方法;通过反复更新参考介质,采用多层次均匀化思路,将本文方法进一步用于多相材料性能的预测.为验证方法的有效性,将预测结果与已有模型结果和试验数据进行对比.结果表明本文方法较已有方法更为合理、有效.当夹杂含量升高时,本文方法较传统有效介质方法的计算精度有所提升.  相似文献   

11.
The transonic unsteady flow of a gas through a cascade of thin, slightly curved plates is quite complex and has received little study. The main difficulties are associated with the nonlinear dependence of the aerodynamic characteristics on the plate thickness. In [1] it is shown that, for a single thin plate performing high-frequency oscillations in a transonic gas stream, the variation of the unsteady aerodynamic characteristics with plate thickness may be neglected. For a plate cascade, the flow pattern is complicated by the aerodynamic interference between the plates, which may depend significantly on their shape. A solution of the problem of transonic flow past a cascade without account for the plate thickness has been obtained by Hamamoto [2].The objective of the present study is the clarification of the dependence of the aerodynamic characteristics of a plate cascade on plate thickness in transonic unsteady flow regimes. The nonlinear equation for the velocity potential is linearized under the assumption that the motionless plate causes significantly greater disturbances in the stream than those due to the oscillations. A similar linearization was carried out for a single plate in [3]. The aerodynamic interference between the plates is determined by the method presented in [4]. As an example, the aerodynamic forces acting on a plate oscillating in a duct and in a free jet are calculated.  相似文献   

12.
研究了亚音速气流下非线性二维薄板结构在横向周期载荷作用下的混沌运动及控制问题。基于von Karman大变形板理论和分离变量法,建立了亚音速下薄板结构的运动控制方程。对于未控系统,采用Melnikov方法判断其混沌运动阈值,并用Runge-Kutta法进行数值验证。对处于混沌运动状态的系统,采用时滞反馈控制方法对混沌运动进行控制。结果表明,Melnikov方法可以有效地预测系统的混沌运动行为,时滞反馈控制方法可以有效地将系统的混沌运动转化为周期运动。  相似文献   

13.
This research presents an experimental investigation into the interaction of a solitary wave and a submerged thin plate under different angles. Experiments are conducted to measure both velocity and vorticity by using the Particle Image Velocimetry (PIV) technique. Effects of changing the thin plate angle on the wave height and wave speed are analyzed through the use of wave height gages. Vortices are generated when the solitary wave is transmitted over the obstacle. Understanding the formation and location of the vortices will help analyze the obstacle effect on the flow. In the initial stage, a thin plate is located vertically, and flow structures are visualized. The plate is then deviated from the vertical direction towards positive angles (the direction of wave propagation) and towards negative angles in the opposite direction. In order to study the effects of the plate angle on the flow structures, experiments are carried out for three positive and three negative angles. Comparison of the formed vortices at different angles shows the formation of an additional vortex near the bottom of the channel for positive angles, as opposed to negative angles. The larger the angle is, the less the formation time of the vortex at the bottom of the channel will be. The study of the clockwise vortices formed behind the obstacle shows that increasing the plate angle in both directions decreases their strength. The clockwise vortices of negative angles are stronger than those of positive angles. In addition, changing the plate angle to the negative direction causes more wave height and wave speed reduction than changing it to the positive direction.  相似文献   

14.
Thin triangular blunt-nosed plate in a viscous hypersonic flow   总被引:1,自引:0,他引:1  
The effect of a small blunt nose on the hypersonic flow past a thin, high-sweep and high-aspect-ratio plate at small incidence is investigated. The analysis is made by means of numerical simulation within the framework of the parabolized Navier-Stokes equations and the Euler equations in combination with approximate methods for calculating the heat transfer. The results are compared with the data of experiments in which some nontrivial features of the heat flux distributions over the thin plate surface were revealed.  相似文献   

15.
The appearance of a local singularity in the solutions for the neighborhood of the trailing edge of a plate in a sub- or supersonic flow makes it necessary to consider the flow in the local region which is described in the first approximation by the Navier-Stokes equations for an incompressible gas. In this paper numerical solutions are obtained for such a region for both a thin plate and a plate with thickness. The streamline patterns and the distributions of the flow functions over the surface of the plate and in the wake behind it are presented. For the plate with finite thickness, a numerical solution is obtained in a wide range of variation of the local Reynolds number.Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 173–176, July–August, 1985.  相似文献   

16.
本文分析了薄膜沿加热平板下落的稳定性。在时间模式下,发现流动的不稳定性是由表面波不稳定和加毛细不稳定构成的,同时当流体的热扩散越大以及界面热量损失越小时,热毛细不稳定越剧烈,在时空模式下,流动随着Marangoni数的增大。流动有可能从对流不稳定过渡到绝对不稳定,这一结论尚待实验验证。  相似文献   

17.
Nominally two-dimensional air flow over a thin flat plate at low Reynolds number is investigated. The primary objective is to experimentally determine with good accuracy the small magnitude lift force, generated by the plate at various angles of attack, by means of application of the Kutta–Joukowsky theorem where circulation is obtained from the line integral of velocity around the flat plate using non-invasive laser doppler velocimeter. Specific focus is on assessing applicability of the Kutta–Joukowsky theorem, originally theorized for inviscid and steady flow, in the post-stall region. At high angles of attack, due to severe flow separation from both the edges of the flat plate and occurrence of periodic vortex shedding, wake flow is found to be highly viscous, turbulent and unsteady. Nevertheless, the results show a remarkably good agreement with previous investigations in both the linear range and the non-linear range of the lift curve without any correction applied to the data. The line integral of velocity along the rectangular loop enclosing the flat plate shows that the vertical components, albeit smaller in magnitude, possess the same sign and hence are additive in contribution to the circulation, whereas the horizontal components possess opposite signs and hence are subtractive in their contribution to the circulation. The paper presents some interesting and hitherto undisclosed features of flow field around the flat plate.  相似文献   

18.
This paper studies the two dimensional flow of an electrically conducting fluid which is an optically thin gray gas past a stationary vertical infinite plate in the presence of radiation. It is assumed that the temperature of the plate and the suction at the plate are constant. The presence of the induced magnetic field is also taken into account. Numerical solutions for the velocity and the induced magnetic field are derived and the effects of the radiation parameter are discussed.  相似文献   

19.

A method of graphic analysis is considered for the calculation of the local thickness of a liquid film in the entrance section of the transformation of slot flow into film flow over a vertical plate. The proposed method can also be used in calculating the local thicknesses of a thin layer during liquid flow over curved surfaces.

  相似文献   

设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号