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国家自然科学基金(11372135)

作品数:7 被引量:19H指数:3
相关作者:陆志良郭同庆唐迪黄炜王远更多>>
相关机构:南京航空航天大学更多>>
发文基金:国家自然科学基金国家重点基础研究发展计划江苏高校优势学科建设工程资助项目更多>>
相关领域:航空宇航科学技术动力工程及工程热物理理学自动化与计算机技术更多>>

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基于k-ε模型的实际地形风场CFD模拟研究被引量:3
2016年
针对风场的数值模拟,采用标准k-ε湍流模型并修正其模型常数,改进入口边界条件的设置,并自定义基于粗糙度长度的z_0类型壁面函数,保证近地面网格的高分辨率。首先以平板地形为计算模型探索和验证以上方法,然后以实际地形Askervein小山为算例进一步验证其应用到工程领域的可行性,即可作为非线性求解器运用在风电场设计的定向计算中。
王远陆志良郭同庆
关键词:风场CFD
A Three-Dimensional Gas-Kinetic BGK Scheme for Simulating Flows in Rotating Machinery
2019年
This paper focuses on the development and application of a threedimensional gas-kinetic Bhatnagar-Gross-Krook(BGK)method for the viscous flows in rotating machinery.For such flows,a rotating frame of reference is usually used in formulating the Navier-Stokes(N-S)equations,and there are two major concerns in constructing the corresponding BGK model.One is the change of the convective velocities in the N-S equations,which can be reflected through modification of the gas streaming velocity.The other one is the necessity to account for the effect of the additional Coriolis and centrifugal forces.Here,a specifically-designed acceleration term is added into the modified Boltzmann equation so that the source effects can be naturally included into the gas evolution process and the resulted fluxes.Under the finitevolume framework,the constructed BGK model is locally solved at each cell interface and then the numerical fluxes can be evaluated.When employing the BGK scheme,it is sometimes found that the calculated spatial derivatives of the initial and equilibrium distribution functions are sensitive to the mesh quality especially in complex rotating flow applications,which may significantly influence flux evaluation.Therefore,an improved approach for computing these slopes is adopted,through which the modeling capability for viscous flows is enhanced.For validation,several numerical examples are presented.The computed results show that the present method can be well applied to a wide range of flows in rotating machinery with favorable accuracy.
Di ZhouZhiliang LuTongqing Guo
An Efficient Dynamic Mesh Generation Method for Complex Multi-Block Structured Grid被引量:2
2014年
Aiming at a complex multi-block structured grid,an efficient dynamic mesh generation method is presented in this paper,which is based on radial basis functions(RBFs)and transfinite interpolation(TFI).When the object is moving,the multi-block structured grid would be changed.The fast mesh deformation is critical for numerical simulation.In this work,the dynamic mesh deformation is completed in two steps.At first,we select all block vertexes with known deformation as center points,and apply RBFs interpolation to get the grid deformation on block edges.Then,an arc-lengthbased TFI is employed to efficiently calculate the grid deformation on block faces and inside each block.The present approach can be well applied to both two-dimensional(2D)and three-dimensional(3D)problems.Numerical results show that the dynamic meshes for all test cases can be generated in an accurate and efficient manner.
Li DingZhiliang LuTongqing Guo
基于多点约束的大展弦比机翼静气动弹性计算被引量:5
2014年
基于雷诺平均N-S方程和多块结构网格技术计算大展弦比机翼的气动力.机翼采用梁模型结构,利用有限元方法计算结构变形.建立基于多点约束(MPC,Multi-Point Constrain)的气动、结构数据的双向传递方法.采用MPC数据插值方法快捷地实现自主研发的计算流体力学(CFD,Computational Fluid Dynamics)程序和NASTRAN计算结构力学(CSD,Computational Structural Dynamics)软件的耦合计算,发展出可以考虑结构非线性的静气动弹性CFD/CSD耦合计算方法,该方法比只考虑单方向变形的柔度法更精确.开展了某大展弦比机翼的静气动弹性数值计算分析,结果显示只考虑机翼纵向变形而忽略展向变形对计算结果会有一定影响,而该算例几何非线性影响较小.
黄炜陆志良唐迪郭同庆
关键词:大展弦比机翼有限元方法N-S方程静气动弹性
大型风力机整机气动弹性响应计算被引量:4
2015年
采用笛卡尔坐标方法描述刚体运动,混合坐标系方法描述弹性体运动和变形,其中弹性变形由模态法表示。通过第一类Lagrange方程推出考虑气动弹性的刚柔混合多体系统的微分-代数方程组,其中代数方程为点和矢量的约束方程。采用Taylor预估、BDF(Backward Differential Formula)校正得到非线性方程组,继而采用Broyden算法求解,从而建立刚柔混合多体系统求解算法。对NH1500风力机进行多体动力学建模,其中机舱、轮毂简化为刚体,塔架、叶片为弹性体,在机舱与轮毂间施加驱动以模拟风力机的定速转动。结合自由涡尾迹的非定常气动力算法,实现考虑气动弹性的大型风力机整机多体动力学响应计算。分析了风剪切和弹性塔架对风力机气动弹性响应的影响,结果表明风剪切会使得叶片振动,而弹性塔架使得风力机响应增加。
唐迪陆志良郭同庆
关键词:气动弹性风力机多体系统动力学
CFD-Based Load Calculation Method for Monopile Support Configuration of Offshore Wind Turbine
2016年
An unsteady load calculation method for the support configuration of a monopile-supported offshore wind turbine is developed based on the Fluent software platform.Firstly,the water wave is generated by imposing the inlet boundary conditions according to the exact potential flow solution.Then the wave evolution is simulated by solving the unsteady incompressible Navier-Stokes(N-S)equations coupled with the volume of fluid method.For the small amplitude wave with reasonable wave parameters,the numerical wave result agrees well with that of the given wave model.Finally,a monopile support configuration is introduced and a CFD-based load calculation method is established to accurately calculate the unsteady load under the combined action of wave and wind.The computed unsteady wave load on a small-size monopile support located in the small amplitude wave flow coincides with that of the Morison formula.The load calculations are also performed on a large-size monopile support and a monopile-supported offshore wind turbine under the combined action of small amplitude wave and wind.
Guo TongqingTong XiaolongLu Zhiliang
大型水平轴风力机叶片气动弹性计算被引量:5
2013年
给出了一种考虑几何非线性的大型风力机静、动气动弹性一体化计算方法.采用涡尾迹方法进行风力机气动载荷计算.建立风力机风轮的三维壳模型.沿周向平均风力机叶片载荷并加载到结构模型进行非线性静气动弹性分析.基于动力学小扰动假设,在静平衡构型下进行动力学线性化,计算风轮固有振动特性.继而结合非定常涡尾迹方法计算风力机动气动弹性响应.计算了NH1500叶片考虑几何非线性的静气动弹性位移和动气动弹性响应.结果表明,大型风力机叶片几何非线性较为明显地减小静气动弹性位移,同时降低动气动弹性的响应幅值.大型风力机气动弹性响应计算需要考虑几何非线性.
唐迪陆志良郭同庆
关键词:风力机气动弹性
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