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悬停旋翼的自由尾迹计算 被引量:5
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作者 徐国华 王适存 《南京航空航天大学学报》 EI CAS CSCD 北大核心 1998年第2期126-131,共6页
在随桨叶旋转的坐标系中,建立了悬停旋翼自由尾迹计算的迭代方法和模型。文中以两种不同的模型旋翼为算例,对叶尖涡的轴向和径向位置进行了计算,并与已有的试验结果进行了对比,检验了模型的可靠性。运用上述自由尾迹模型,分别研究... 在随桨叶旋转的坐标系中,建立了悬停旋翼自由尾迹计算的迭代方法和模型。文中以两种不同的模型旋翼为算例,对叶尖涡的轴向和径向位置进行了计算,并与已有的试验结果进行了对比,检验了模型的可靠性。运用上述自由尾迹模型,分别研究了不同叶尖马赫数、桨距角和桨叶片数时悬停尾迹形状的变化,表明了旋翼参数对自由尾迹形状的影响。最后,文末给出了一些结论。 展开更多
关键词 直升机 旋翼 尾流 旋翼空气动力学 涡元 自由尾迹
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Identification of hydrodynamic coefficients from experiment of vortex-induced vibration of slender riser model 被引量:5
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作者 TANG GuoQiang LU Lin +3 位作者 TENG Bin PARK HanI1 SONG JiNing ZHANG JianQiao 《Science China(Technological Sciences)》 SCIE EI CAS 2011年第7期1894-1905,共12页
One of the challenges in predicting the dynamic response of deepwater risers under vortex-induced vibration (VIV) is that it runs short of believable fluid loading model. Moreover, the hydrodynamic loading is also d... One of the challenges in predicting the dynamic response of deepwater risers under vortex-induced vibration (VIV) is that it runs short of believable fluid loading model. Moreover, the hydrodynamic loading is also difficult to be measured directly in the VIV experiments without disturbing the fluid field. In the present work, by means of a finite element analysis method based on the experimental data of the response displacements, the total instantaneous distributions of hydrodynamic forces together with the hydrodynamic coefficients on the riser model with large aspect ratio (length/ddiameter) of 1750 are achieved. The steady current speeds considered in the experiments of this work are ranging from 0.15 rn/s to 0.60 m/s, giving the Reynolds Number between 2400 and 9600. The hydrodynamic coefficients are evaluated at the fundamental frequency and in the higher order frequency components for both in-line and cross-flow directions. It is found that the Root-Mean Squared hydrodynamic forces of the higher order response frequency are larger than those of the fundamental response frequency. Negative lift or drag coefficients are found in the numerical results which is equivalent to the effect of fluid damping. 展开更多
关键词 vortex-induced vibration deepwater riser hydrodynamic coefficients finite element method dynamic response
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尾涡数值模拟的曲涡元技术 被引量:2
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作者 楼武畺 王适存 《空气动力学学报》 CSCD 北大核心 1990年第4期459-463,共5页
连接涡线端点形成涡段并计算其对空间任意点的影响系数是尾迹分析的基本环节,称为涡元技术。本文推出圆弧涡元与其应用程序,并引进抛物拱弧涡元,以代替传统的直涡元。提供的曲涡元程序可方便地用于尾迹分析,算例表明曲涡元在提高精度减... 连接涡线端点形成涡段并计算其对空间任意点的影响系数是尾迹分析的基本环节,称为涡元技术。本文推出圆弧涡元与其应用程序,并引进抛物拱弧涡元,以代替传统的直涡元。提供的曲涡元程序可方便地用于尾迹分析,算例表明曲涡元在提高精度减少计算量方面的先进性。 展开更多
关键词 尾涡 曲涡元 数值模拟 诱导速度
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NUMERICAL SIMULATION OF UNSTEADY-STATE UNDEREXPANDED JET USING DISCONTINUOUS GALERKIN FINITE ELEMENT METHOD 被引量:3
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作者 陈二云 李志刚 +3 位作者 马大为 乐贵高 赵改平 任杰 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 2008年第2期89-93,共5页
A discontinuous Galerkin finite element method (DG-FEM) is developed for solving the axisymmetric Euler equations based on two-dimensional conservation laws. The method is used to simulate the unsteady-state underex... A discontinuous Galerkin finite element method (DG-FEM) is developed for solving the axisymmetric Euler equations based on two-dimensional conservation laws. The method is used to simulate the unsteady-state underexpanded axisymmetric jet. Several flow property distributions along the jet axis, including density, pres- sure and Mach number are obtained and the qualitative flowfield structures of interest are well captured using the proposed method, including shock waves, slipstreams, traveling vortex ring and multiple Mach disks. Two Mach disk locations agree well with computational and experimental measurement results. It indicates that the method is robust and efficient for solving the unsteady-state underexpanded axisymmetric jet. 展开更多
关键词 jets computational fluid dynamics multiple Mach disks vortex ring discontinuous Galerkin finite element method
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薄矩形柱绕流旋涡脱落的抑制 被引量:1
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作者 邵传平 林建忠 魏庆鼎 《力学学报》 EI CSCD 北大核心 2010年第4期615-622,共8页
用窄条形控制件对截面宽度为B,厚度为H的矩形柱体绕流的旋涡脱落进行抑制.实验在风洞中进行,实验范围为B/H=2.0~5.0,Re=V∞H/ν=3.75×10^3~1.05×10^4.矩形柱的宽边B与来流平行,窄条与柱体等长,且两者轴线相互平行放置.窄条... 用窄条形控制件对截面宽度为B,厚度为H的矩形柱体绕流的旋涡脱落进行抑制.实验在风洞中进行,实验范围为B/H=2.0~5.0,Re=V∞H/ν=3.75×10^3~1.05×10^4.矩形柱的宽边B与来流平行,窄条与柱体等长,且两者轴线相互平行放置.窄条宽度为b/H=0.5,窄条厚度远小于其宽度;窄条位置可变,但窄条表面保持与来流垂直.尾流脉动速度测量和流动显示结果表明:当窄条位于一个有效区内时,矩形柱体两侧的旋涡脱落被抑制;而当窄条位于一个单侧有效区内时,矩形体一侧的旋涡脱落被抑制,在另一侧旋涡脱落却仍存在.有效区范围从矩形体的上游某点一直延续到矩形体的下游某点.单侧有效区将整个有效区围在其中.有效区和单侧有效区范围随着B/H的增大而增大,但随着Re的增大而减小. 展开更多
关键词 抑制 涡脱落 矩形柱 控制件 实验
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Nonlinear Numerical Analysis of Vortex-Induced Vibration of A Three-Dimensional Deepwater Steep Wave Riser with Large Deformation Features 被引量:1
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作者 CHENG Yong SONG Fu-kai LI Ming-xin 《China Ocean Engineering》 SCIE EI CSCD 2022年第4期601-613,共13页
The cross-flow(CF)vortex-induced vibration(VIV)of a deepwater steep wave riser(SWR)subjected to uniform or shear flow loads is investigated numerically.The model is based on a three-dimensional(3D)nonlinear elastic ro... The cross-flow(CF)vortex-induced vibration(VIV)of a deepwater steep wave riser(SWR)subjected to uniform or shear flow loads is investigated numerically.The model is based on a three-dimensional(3D)nonlinear elastic rod theory coupled with a wake oscillator model.In this numerical simulation,the nonlinear motion equations of the riser with large deformation features are established in a global coordinate system to avoid the transformation between global and local coordinate systems,and are discretized with the time-domain finite element method(FEM).A wakeoscillator model is employed to study the vortex shedding,and the lift force generated by the wake flow is described in a van der Pol equation.A Newmark-βiterative scheme is used to solve their coupling equation for the VIV response of the SWR.The developed model is validated against the existing experimental results for the VIV response of the top-tension riser(TTR).Then,the numerical simulations are executed to determine VIV characteristics of the SWR.The effects of both flow velocity and the spanwise length of the flow field on the drag coefficient in the inline(IL)direction and the lift coefficient in the CF direction are investigated systematically.The results indicate that compared with TTR,the low frequency and multi-modal vibration are the main components of the SWR due to the large deformation and flexible characteristics.For shear flow,the multi-frequency resonance dominates the VIV response of the SWR,especially at the hang-off segment. 展开更多
关键词 steep wave riser vortex-induced vibration time domain simulation nonlinear finite element wake oscillator
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小控制杆对矩形柱尾流旋涡脱落的抑制 被引量:2
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作者 郑博文 邵传平 张洪军 《中国计量学院学报》 2011年第3期228-236,共9页
采用小控制杆方法对主柱宽厚比B/H为2.0和3.0的两种矩形柱尾流的旋涡脱落进行了抑制实验.实验在风洞中进行,雷诺数(Re)范围为1.5×103至5.5×103,控制杆与矩形柱长度相同,两者相互平行放置.对三种不同宽度的控制杆进行了实验,... 采用小控制杆方法对主柱宽厚比B/H为2.0和3.0的两种矩形柱尾流的旋涡脱落进行了抑制实验.实验在风洞中进行,雷诺数(Re)范围为1.5×103至5.5×103,控制杆与矩形柱长度相同,两者相互平行放置.对三种不同宽度的控制杆进行了实验,小杆宽厚比分别为b/H=0.2,0.32和0.4.流动显示和热线测量结果表明:在柱体附近存在一个有效区,控制杆位于此区内时,柱体两侧的旋涡脱落被抑制.另外还存在一个单侧有效区,当控制杆位于该区内时,柱体一侧的旋涡脱落被抑制,而另一侧未被抑制,形成"单侧旋涡脱落现象".文中还研究了小杆宽厚比、矩形柱宽厚比和雷诺数对有效区和单侧有效区的影响,发现b/H增大时,有效区和单侧有效区不是扩大,而是有所缩小;当B/H增大时,有效区和单侧有效区扩大,而且有效区由一个变为两个;Re增大时,有效区和单侧有效区略有缩小. 展开更多
关键词 流动控制 旋涡脱落 矩形柱 控制杆
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High efficiency and broad bandwidth terahertz vortex beam generation based on ultra-thin transmission Pancharatnam-Berry metasurfaces 被引量:2
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作者 Wenyu Li Guozhong Zhao +2 位作者 Tianhua Meng Ran Sun Jiaoyan Guo 《Chinese Physics B》 SCIE EI CAS CSCD 2021年第5期667-672,共6页
The terahertz(THz)vortex beam generators are designed and theoretically investigated based on single-layer ultra-thin transmission metasurfaces.Noncontinuous phase changes of metasurfaces are obtained by utilizing Pan... The terahertz(THz)vortex beam generators are designed and theoretically investigated based on single-layer ultra-thin transmission metasurfaces.Noncontinuous phase changes of metasurfaces are obtained by utilizing Pancharatnam-Berry phase elements,which possess different rotation angles and are arranged on two concentric rings centered on the origin.The circularly polarized incident THz beam could be turned into a cross-polarization transmission wave,and the orbital angular momentum(OAM)varies in value by lh.The l values change from±1 to±5,and the maximal cross-polarization conversion efficiency that could be achieved is 23%,which nearly reaches the theoretical limit of a single-layer structure.The frequency range of the designed vortex generator is from 1.2 THz to 1.9 THz,and the generated THz vortex beam could keep a high fidelity in the operating bandwidth.The propagation behavior of the emerged THz vortex beam is analyzed in detail.Our work offers a novel way of designing ultra-thin and single-layer vortex beam generators,which have low process complexity,high conversion efficiency and broad bandwidth. 展开更多
关键词 metasurface terahertz vortex beam Pancharatnam-Berry phase element conversion efficiency
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Kenics型静态混合器性能优化的数值与应用分析 被引量:2
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作者 权登辉 杨晓军 +2 位作者 刘龙 华绍广 汪洋 《化工机械》 CAS 2021年第2期203-208,228,共7页
采用计算流体力学方法研究了旋流元件对静态混合器内气相流场分布和混合性能的影响。结果表明:旋流元件的加入有效降低了管路外缘处气流切向速度和径向压强分布,管内流场分布较为均匀,其中以旋流元件数N=6时最为明显;在353K的管壁加热... 采用计算流体力学方法研究了旋流元件对静态混合器内气相流场分布和混合性能的影响。结果表明:旋流元件的加入有效降低了管路外缘处气流切向速度和径向压强分布,管内流场分布较为均匀,其中以旋流元件数N=6时最为明显;在353K的管壁加热温度下,速度均方根值再次降低,明显提高了管内气相组分的质量分数均匀性。 展开更多
关键词 旋流元件 静态混合器 气相流场 数值模拟
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Numerical investigation on fluid forces of piggyback circular cylinders in tandem arrangement at low Reynolds numbers 被引量:1
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作者 Linfeng Chen Yuhong Dong 《Acta Mechanica Sinica》 SCIE EI CAS CSCD 2021年第4期599-612,I0002,共15页
Numerical simulations of flows past the piggyback circular cylinders in tandem arrangement are performed by solving the variational multiscale formulation of the incompressible Navier-Stokes equations using in-house f... Numerical simulations of flows past the piggyback circular cylinders in tandem arrangement are performed by solving the variational multiscale formulation of the incompressible Navier-Stokes equations using in-house finite element method(FEM)codes.The effects of the gap-spacing-to-diameter(G/D)and the two diameter ratio(d/D)on the flow characteristics and the reductions of the root-mean-square(RMS)drag and lift coefficients are considered for Reynolds numbers(Res)are 100 and 200.The validation shows the fluid force coefficients obtained by the in-house FEM codes are in good agreement with the results in the existing literatures.The obtained results show that,with a proper placement of the smaller cylinder(d/D=0.2)behind the larger cylinder,the RMS drag and lift coefficients largely decrease compared to those of the single circular cylinder.When d/D=0.2,the largest reductions of the RMS lift coefficient of the larger cylinder and the RMS total lift coefficient appear at G/D=1.2 as Re=100 and at G/D=1.0 as Re=200.It is observed that the proper placement of the smaller cylinder causes the surrounding vorticity to take opposite sign with the vorticity in the outer region so as to suppress and postpone the vortex shedding in the wake,and that the different positions of the vortex shedding at two Res cause that the largest reductions of the RMS lift coefficient of the larger cylinder and the RMS total lift coefficient appear at different G/D as Re is different.When d/D varies,the variation of the RMS total lift coefficient behaves differently at two Res.It decreases with J/D increasing at Re=100,while it no longer monotonously varies with J/D,but reaches a minimum in the considered range of d/D at Re=200.Moreover,the larger d/D results in stronger suppression and postponement of the vortex shedding in the wake. 展开更多
关键词 Piggyback circular cylinders Hydrodynamic forces vortex shedding Finite element method Variational multiscale method
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Nonlinear Analysis of Bidirectional Vortex-Induced Vibration of A Deepwater Steep Wave Riser Subjected to Oblique Currents
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作者 CHENG Yong TANG Lian-yang JI Chun-yan 《China Ocean Engineering》 SCIE EI CSCD 2021年第6期852-865,共14页
An improved three-dimensional(3D)time-domain couple model is established in this paper to simulate the bidirectional vortex-induced vibration(VIV)of a deepwater steep wave riser(SWR)subjected to oblique currents.In th... An improved three-dimensional(3D)time-domain couple model is established in this paper to simulate the bidirectional vortex-induced vibration(VIV)of a deepwater steep wave riser(SWR)subjected to oblique currents.In this model,the nonlinear motion equations of the riser are established in the global coordinate system based on the slender rod theory with the finite element method.Van der Pol equations are used to describe the lift forces induced by the x-and y-direction current components,respectively.The coupled equations at each time step are solved by a Newmark-βiterative scheme for the SWR VIV.The present model is verified by comparison with the published experimental results for a top-tension riser.Then,a series of simulations are executed to determine the influences of the oblique angle/velocity of the current,different top-end positions and the length of the buoyancy segment on the VIV displacement,oscillating frequency as well as hydrodynamic coefficients of the SWR.The results demonstrate that there exists a coupled resonant VIV corresponding to x-direction and y-direction,respectively.However,the effective frequency is almost identical between the vibrations at the hang-off segment along x and y directions.The addition of the buoyancy modules in the middle of the SWR has a beneficial impact on the lift force of three segments and simultaneously limits the VIV response,especially at the decline segment and the hang-off segments.Additionally,the incident current direction significantly affects the motion trajectory of the SWR which mainly includes the fusiform and rectangle shapes. 展开更多
关键词 steep wave riser(SWR) bidirectional vortex-induced vibration wake oscillator model time-domain finite element method(TDFEM)
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Numerical Study of Quantized Vortex Interaction in theGinzburg-Landau Equation on Bounded Domains
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作者 Weizhu Bao Qinglin Tang 《Communications in Computational Physics》 SCIE 2013年第8期819-850,共32页
In this paper,we study numerically quantized vortex dynamics and their interaction in the two-dimensional(2D)Ginzburg-Landau equation(GLE)with a dimensionless parameter#>0 on bounded domains under either Dirichlet ... In this paper,we study numerically quantized vortex dynamics and their interaction in the two-dimensional(2D)Ginzburg-Landau equation(GLE)with a dimensionless parameter#>0 on bounded domains under either Dirichlet or homogeneous Neumann boundary condition.We begin with a reviewof the reduced dynamical laws for time evolution of quantized vortex centers in GLE and show how to solve these nonlinear ordinary differential equations numerically.Then we present efficient and accurate numerical methods for discretizing the GLE on either a rectangular or a disk domain under either Dirichlet or homogeneous Neumann boundary condition.Based on these efficient and accurate numerical methods for GLE and the reduced dynamical laws,we simulate quantized vortex interaction of GLE with different#and under different initial setups including single vortex,vortex pair,vortex dipole and vortex lattice,compare them with those obtained from the corresponding reduced dynamical laws,and identify the cases where the reduced dynamical laws agree qualitatively and/or quantitatively as well as fail to agree with those from GLE on vortex interaction.Finally,we also obtain numerically different patterns of the steady states for quantized vortex lattices under the GLE dynamics on bounded domains. 展开更多
关键词 Ginzburg-Landau equation quantized vortex Dirichlet boundary condition homogeneous Neumann boundary condition reduced dynamical laws time splitting compact finite differencemethod finite element method
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解Oseen方程的P_1非协调四边形单元的涡旋粘性法
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作者 左芳芳 孔花 刘程熙 《四川师范大学学报(自然科学版)》 CAS CSCD 北大核心 2012年第5期632-638,共7页
解Oseen方程最主要的方法是混合有限元法,而这需要混合有限元空间满足离散的inf-sup(LBB)条件以及克服对流占优以防止数值解产生伪振荡.所采取的四边形网格上的P1-Q0元的非协调稳定化方法是通过L2局部投影添加涡旋粘性项来修正变分形式... 解Oseen方程最主要的方法是混合有限元法,而这需要混合有限元空间满足离散的inf-sup(LBB)条件以及克服对流占优以防止数值解产生伪振荡.所采取的四边形网格上的P1-Q0元的非协调稳定化方法是通过L2局部投影添加涡旋粘性项来修正变分形式,增强其格式的稳定性,以绕开LBB条件,并克服对流占优.同时通过局部投影稳定化分析与最优误差估计,在理论上论证此方法的收敛性,使得P1非协调四边形元的应用更为广泛. 展开更多
关键词 Oseen方程 涡旋粘性 非协调 四边形元
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CONVERGENCE OF VORTEX WITH BOUNDARY ELEMENT METHODS
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作者 P.W. Zhang(Department of Mathematics, Peking University) 《Journal of Computational Mathematics》 SCIE CSCD 1997年第2期127-137,共11页
In this work, the vortex methods for Euler equations with initial boundary value problem is considered, Poisson equations are solved using boundary element methods which can be seen to require less operations to compu... In this work, the vortex methods for Euler equations with initial boundary value problem is considered, Poisson equations are solved using boundary element methods which can be seen to require less operations to compute the velocity field from the vorticity by Chorin([6]). We prove that the rate of convergence of the boundary element schemes can be independent of the vortex blob parameters. 展开更多
关键词 MATH CONVERGENCE OF vortex WITH BOUNDARY element METHODS ZHANG
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窄条控制件对旋转振荡板尾流的控制
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作者 魏婷婷 邵传平 《中国计量学院学报》 2014年第4期391-397,共7页
两个小窄条对称地放于两侧,对宽厚比B/H=3的旋转振荡平板的尾流旋涡脱落进行抑制.板在平行于来流位置附近绕对称轴作旋转振荡,振幅为10°.窄条长边与板的旋转轴平行,窄条表面与来流方向垂直,窄条宽度与板的厚度之比b/H=1/3.控制参... 两个小窄条对称地放于两侧,对宽厚比B/H=3的旋转振荡平板的尾流旋涡脱落进行抑制.板在平行于来流位置附近绕对称轴作旋转振荡,振幅为10°.窄条长边与板的旋转轴平行,窄条表面与来流方向垂直,窄条宽度与板的厚度之比b/H=1/3.控制参数为窄条位置.尾流流动显示图片和尾流脉动速度谱结果表明,当窄条位于有效区域内时,板两侧的涡脱落得到有效抑制.有效区尺度随着无量纲频率的增大而增大,随着雷诺数的增大而减小. 展开更多
关键词 旋转振荡平板 旋涡脱落 流动控制 控制件
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拖式吊舱螺旋桨定常性能理论计算 被引量:12
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作者 陈飞笑 杨晨俊 《水动力学研究与进展(A辑)》 CSCD 北大核心 2003年第4期515-520,共6页
本文提出拖式吊舱螺旋桨 (螺旋桨位于吊舱首部 )定常水动力性能的势流理论计算方法。螺旋桨采用升力面理论涡格法、吊舱采用面元法分析计算 ,二者的相互干扰通过叠代计算来处理。考虑吊舱的影响 ,修改了尾涡模型。应用本方法 ,计算了拖... 本文提出拖式吊舱螺旋桨 (螺旋桨位于吊舱首部 )定常水动力性能的势流理论计算方法。螺旋桨采用升力面理论涡格法、吊舱采用面元法分析计算 ,二者的相互干扰通过叠代计算来处理。考虑吊舱的影响 ,修改了尾涡模型。应用本方法 ,计算了拖式吊舱螺旋桨的定常性能 ,并与空泡水筒试验结果进行了比较 。 展开更多
关键词 拖式吊舱螺旋桨 定常水动力性能 计算方法 船舶 势流理论 涡格法 面元法 叠代计算 尾涡模型
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开口叠合梁断面气动性能的试验研究 被引量:21
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作者 战庆亮 周志勇 葛耀君 《桥梁建设》 EI CSCD 北大核心 2017年第1期17-22,共6页
钢-混叠合梁开口断面由于其外形的钝体特征,易出现气动稳定性问题,为了有效抑制开口断面的颤振和涡振,对其断面外形进行优化,以4座采用钢-混叠合梁开口断面的桥梁(鄱阳湖大桥和香溪河大桥为双塔斜拉桥,鳌江四桥为独塔斜拉桥,鹦鹉洲长江... 钢-混叠合梁开口断面由于其外形的钝体特征,易出现气动稳定性问题,为了有效抑制开口断面的颤振和涡振,对其断面外形进行优化,以4座采用钢-混叠合梁开口断面的桥梁(鄱阳湖大桥和香溪河大桥为双塔斜拉桥,鳌江四桥为独塔斜拉桥,鹦鹉洲长江大桥为三塔悬索桥)为例,通过有限元计算和节段模型风洞试验研究其动力特性,分析开口断面的颤振性能和涡振性能,并寻找合理有效的抑振措施。结果表明:增加风嘴可以显著提高断面的颤振稳定性;下表面增设稳定板可以显著提高颤振临界风速;增加风嘴可以有效抑制开口断面的涡振,增大风嘴结构尺寸后抑振效果更加明显,开口断面增设挑梁结构可以显著改善涡振稳定性。 展开更多
关键词 钢-混叠合梁 气动性能 颤振 涡振 有限元法 风洞试验 风嘴
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基于热应力场耦合的涡旋压缩机动涡盘有限元分析 被引量:18
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作者 殷俊 杨美传 冯鉴 《压缩机技术》 2011年第6期6-9,共4页
通过采用有限元方法,运用ANSYS软件,对涡旋压缩机动涡盘受气体力载荷工况和受温度载荷、气体力载荷共同作用工况时进行比较分析,并做不同温度载荷下的耦合分析,得出动涡盘变形和应力分布规律,指出了设计分析中应考虑的重要因素。
关键词 动涡盘 有限元方法 热应力 耦合分析
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虚拟风场和风力机模拟系统的实验研究 被引量:17
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作者 窦真兰 王晗 +2 位作者 张秋琼 凌志斌 蔡旭 《中国电机工程学报》 EI CSCD 北大核心 2011年第20期127-135,共9页
在不具备风场环境或风力机的条件下,建立虚拟风场和风力机模拟系统,对风力发电系统的研究具有重要作用。根据风速变化规律,建立了基于谱密度分析的自回归理论的风速模型。在此风速模型基础上,考虑涡流效应,对叶片进行受力分析,根据叶素... 在不具备风场环境或风力机的条件下,建立虚拟风场和风力机模拟系统,对风力发电系统的研究具有重要作用。根据风速变化规律,建立了基于谱密度分析的自回归理论的风速模型。在此风速模型基础上,考虑涡流效应,对叶片进行受力分析,根据叶素理论和权系数分配叶素的方法建立风轮转矩模型,利用转矩控制直流电动机模拟风力机,搭建了虚拟风场和风力机模拟系统实验平台。虚拟风场的建立为虚拟风力机暂态或连续性实验提供了良好的基础。风力机模拟系统实验不仅验证了风轮转矩模型的准确性,反映了风速变化时模拟输出风轮转矩的快速跟随性能,而且可用于变速恒频风力发电系统的研究,证明其控制策略的正确性。 展开更多
关键词 虚拟风场 自回归理论 风轮转矩 涡流效应 叶素理论 权系数分配 风力机模拟系统
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超深水钻井隔水管-井口系统涡激振动疲劳分析 被引量:17
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作者 孙友义 鞠少栋 +1 位作者 蒋世全 陈国明 《石油学报》 EI CAS CSCD 北大核心 2011年第6期1050-1054,共5页
超深水钻井作业经常发生隔水管涡激疲劳问题,而由隔水管涡激振动(VIV)引起的井口系统疲劳可能更为严重。根据超深水隔水管-井口系统VIV疲劳分析算法与计算流程,建立隔水管-井口系统整体有限元模型,通过模态分析提取各阶模态下所有节点... 超深水钻井作业经常发生隔水管涡激疲劳问题,而由隔水管涡激振动(VIV)引起的井口系统疲劳可能更为严重。根据超深水隔水管-井口系统VIV疲劳分析算法与计算流程,建立隔水管-井口系统整体有限元模型,通过模态分析提取各阶模态下所有节点的振型、斜率和曲率,应用SHEAR7程序进行详细疲劳分析,识别系统关键疲劳部位,评估系统的VIV疲劳寿命,并研究顶张力、防喷器(BOP)、导管结构尺寸及井口出泥高度对井口系统VIV疲劳特性的影响规律。针对南海某超深水井的隔水管-井口系统进行实例分析,结果表明,超深水隔水管-井口系统容易发生多阶模态振动,系统最大疲劳损伤位于导管上,系统疲劳寿命满足作业要求,适当提高顶张力、采用小型化的BOP、增大导管抗弯刚度以及降低井口出泥高度均可有效改善井口系统的VIV疲劳性能。 展开更多
关键词 超深水 钻井隔水管 井口 导管 涡激振动 疲劳分析 有限元分析
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