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离心泵启动过程内部瞬态流动的二维数值模拟 总被引:6,自引:3,他引:3
为分析离心泵启动过程外部瞬态特性的内流机理,建立求解叶轮启动和加速过程泵内部非定常流动的数值模拟方法,以二维离心泵为模型进行启动过程内部流动的数值模拟研究.以绝对坐标系描述伞场流动,采用动网格方法实现离心泵启动过程中叶轮加速旋转引起的流场变形,选用人涡模拟(LES)描述湍流.分析了叶轮启动过程巾内部非定常流动结构和演化过程及其与外部瞬态特性的关系,并与准稳态假设下的流动模拟结果进行了对比分析,定性地分析了离心泵在启动过程中的瞬态效应,验证了采用动网格方法求解启动过程瞬态流动的可行性. 相似文献
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低速轴流涡轮非定常数值模拟的非线性谐波法 总被引:4,自引:0,他引:4
本文介绍了旋转机械非定常数值模拟的非线性谐波方法,并对某低速轴流涡轮的流场进行了数值模拟,获得了该涡轮通道内的非定常流场结构.在与实验结果及定常计算结果对比确认的基础上,分析了该涡轮动静叶间干涉与非定常流动特性,并比较了谐波阶数和工质的压缩性对计算结果的影响.研究结果表明,非线性谐波方法可有效地模拟动静非定常干涉. 相似文献
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本文采用时空守恒(CE/SE)格式求解Navier-Stoks方程与Euler方程,数值模拟了绕圆柱流动引发的气动噪声源及传播问题.对近声场与远声场采用了不同的控制方程和边界条件,分别得到了流场与声场解.将其与采用大涡模拟和FW-H方程得到的结果进行了对比,表明本文的数值方法能够很好地反映流场与声场的形态,能较好地模拟声场指向性及流场中的拟声现象,相比LES/FW-H方法能更精确地反映流场与声场的相互关系. 相似文献
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谐波平衡法是一种高效周期性非定常流动频域计算方法.本文研究可变周期谐波平衡法,通过求解Navier-Stokes方程模拟低速不可压条件下的二维钝体绕流周期性非定常涡脱落问题.对于这类流动变化周期未知的非定常问题,将涡脱落周期T作为变量,采用基于残差导数的可变周期计算方法推进求解.以圆柱绕流和方柱绕流为例,研究考察了谐波平衡法的计算精度和效率,并分析研究了不同参数对计算结果的影响.针对圆柱绕流问题,采用三种不同优化方法进行周期T的迭代计算,对比研究了它们的计算精度和效率.计算结果表明:谐波平衡法采用3个谐波数就可以准确模拟周期性非定常涡脱落问题,辨识的涡脱落频率和阻力系数与实验值及其他数值结果一致,与时域方法相比该方法具有较高的计算效率.不同优化方法的计算结果相同,共轭梯度法和牛顿法的收敛速度与最速下降法采用较大搜索步长时的收敛速度一致.由于牛顿法没有参数问题,因此该方法在工程计算中更有优势. 相似文献
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本文继Zheng-huan Teng[1]中介绍的解Navier-stokes方程的椭圆涡团法,研究了一种新的变形涡团法,用以模拟不可压粘性流体绕圆柱的不定常流动。圆柱在静止流体中突然起动并做匀速直线运动。对整个流动区域构造完全Navier-Stokes方程的解并不容易,近十年出现很多数值研究,本文对算法有所推进。把本文的方法称作变形涡团法是因为圆柱边界附近的流体中用椭圆涡团,远离边界时用圆形涡团。计算圆柱绕流比平板绕流在满足附着条件上更为困难,本文分析了怎样在圆柱边界上给出适当的附着条件的数值方法。在算例中雷诺数分别取200、550、3000,得到了不定常边界层分离,二次涡等复杂的物理现象,这些数值结果与近年实验结果[2]是一致的。 相似文献
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A grid-free high-resolution spatially-adaptive vortex method for two-dimensional incompressible flow in bounded domains is presented. The computational algorithm is based on operator splitting in which convection and diffusion are handled separately every time step. In the convection step, computational elements are convected with velocities obtained by fast approximations of the Biot–Savart superposition with second-order Runge–Kutta time integration scheme. Diffusion is performed using the smooth redistribution method that employs a Gaussian basis function for vorticity in the interior. Near solid walls, the core functions are modified to conserve circulation. The no-slip boundary condition is enforced by creating of a vortex sheet that is redistributed to neighboring elements using the redistribution method. The proposed method enables accurate and smooth recovery of the vorticity and does not require explicit use of vortex images or occasional re-meshing. Algorithms for reduction in computational cost by accurately removing elements in overcrowded regions and for spatial adaptivity that allows for variable core sizes and variable element spacing are presented. Computations of flow around an impulsively started cylinder for Reynolds number values of 1000, 3000, and 9500 are preformed to investigate various aspects of the proposed method. 相似文献
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We present a generalization of the no-slip boundary condition by Lätt et al. [J. Lätt, B. Chopard, O. Malaspinas, M. Deville, A. Michler, Straight velocity boundaries in the lattice Boltzmann method, Physical Review E 77 (5) (2008) 056703] from straight to curved geometries for the lattice Boltzmann Bhatnager–Gross–Krook method (LBGK). The boundary condition is based on a reconstruction of the populations from the density, velocity and rate of strain. For curved boundaries, the reconstruction reduces the question of accuracy to a technical issue of interpolation. We present a method of interpolation allowing a very accurate representation of the curved boundary. The resulting boundary condition is verified for three different test cases: Taylor–Couette flow in-between rotating cylinders, laminar flow around a cylinder and flow past an impulsively started cylinder, demonstrating its second order accuracy and low error constant. The present boundary is stable for relaxation frequencies close to two. 相似文献
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G. Palani 《Journal of Engineering Thermophysics》2012,21(4):259-277
Numerical modeling of two-dimensional, unsteady, laminar, isothermal heat and mass transfer by MHD free convection flow past an impulsively started vertical cylinder in the presence of Dufour and Soret effects is considered. The governing equations of the flow problems, valid in the free convection regime, are transformed into a nondimensional form using appropriate nondimensional parameters. These equations are solved numerically by an efficient, implicit, iterative, finite-difference scheme of Crank-Nicolson type. A parametric study illustrating the influence of the magnetic field, Grashof number, and the Dufour and Soret numbers on the fluid velocity, temperature, and concentration, as well as the local and average skin friction, Nusselt and Sherwood numbers is conducted. The obtained results are shown graphically and the physical aspects of the problem are discussed. 相似文献
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Alexandre Dupuis Philippe Chatelain Petros Koumoutsakos 《Journal of computational physics》2008,227(9):4486-4498
We present a lattice-Boltzmann method coupled with an immersed boundary technique for the simulation of bluff body flows. The lattice-Boltzmann method for the modeling of the Navier–Stokes equations, is enhanced by a forcing term to account for the no-slip boundary condition on a non-grid conforming boundary. We investigate two alternatives of coupling the boundary forcing term with the grid nodes, namely the direct and the interpolated forcing techniques. The present LB–IB methods are validated in simulations of the incompressible flow past an impulsively started cylinder at low and moderate Reynolds numbers. We present diagnostics such as the near wall vorticity field and the drag coefficient and comparisons with previous computational and experimental works and assess the advantages and drawbacks of the two techniques. 相似文献
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从Lagrangian角度数值分析了圆柱瞬时起动过程中的非定常瞬态流动现象,如分离泡产生、破裂和涡脱落等及其产生的非定常效应,揭示了所列现象诱导的物质输运和迁移效应,首先采用双时间步长的特征线算子分裂算法数值模拟了圆柱起动过程中的瞬时流场,然后采用数值方法从流场中提取出Lagrangian拟序结构(LCSs),并根据非线性动力学理论研究了流动分离和旋涡演化过程中的物质输运作用,结果表明,圆柱瞬时起动后所产生的非定常阻力与相应瞬态现象中的物质输运有密切的关系:对称分离泡产生及其在流向方向的生长,能够使分离泡内压力升高且分布均匀,从而减小阻力;对称分离泡的失稳增强了分离泡与主流之间的物质输运作用,最终导致涡的脱落,并有利于推迟流动分离和减小分离区域,非定常流动中LCSs所描述的物质输运和迁移作用对流动控制的机理研究具有一定指导意义。 相似文献
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An immersed boundary method for the incompressible Navier–Stokes equations in irregular domains is developed using a local ghost cell approach. This method extends the solution smoothly across the boundary in the same direction as the discretization it will be used for. The ghost cell value is determined locally for each irregular grid cell, making it possible to treat both sharp corners and thin plates accurately. The time stepping is done explicitly using a second order Runge–Kutta method. The spatial derivatives are approximated by finite difference methods on a staggered, Cartesian grid with local grid refinements near the immersed boundary. The WENO scheme is used to treat the convective terms, while all other terms are discretized with central schemes. It is demonstrated that the spatial accuracy of the present numerical method is second order. Further, the method is tested and validated for a number of problems including uniform flow past a circular cylinder, impulsively started flow past a circular cylinder and a flat plate, and planar oscillatory flow past a circular cylinder and objects with sharp corners, such as a facing square and a chamfered plate. 相似文献