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解三维水翼绕流的下潜涡环栅格法 被引量:8
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作者 陈材侃 刘华 《船舶力学》 EI 北大核心 2005年第2期41-45,共5页
在包含于机翼表面内的某次表面及尾涡面上分布法向偶极子,在翼面上满足物面边界条件,建立了解三维机翼绕流的下潜涡环栅格法。考虑到非线性的自由液面边界条件,用下潜涡环栅格法求解水翼绕流问题。通过算例验证了方法的正确性和程序的... 在包含于机翼表面内的某次表面及尾涡面上分布法向偶极子,在翼面上满足物面边界条件,建立了解三维机翼绕流的下潜涡环栅格法。考虑到非线性的自由液面边界条件,用下潜涡环栅格法求解水翼绕流问题。通过算例验证了方法的正确性和程序的可靠性。本方法可用于水翼及水下安定翼和各种舵的水动力计算。 展开更多
关键词 水翼 绕流 下潜栅格 非线性 液面边界条件
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基于涡环栅格法的三体船斜拖水动力数值分析
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作者 王鸿东 易宏 余平 《舰船科学技术》 北大核心 2018年第4期22-26,共5页
以三体船的操纵性能预报为背景,基于势流理论的三维面元法,对三体船的斜拖运动进行数值模拟,并求得相应的水动力系数。将传统的运用于机翼升力计算的涡环栅格法(VLM)运用于三体船斜拖运动的数值模拟,船体表面被离散成四边形的网格,网格... 以三体船的操纵性能预报为背景,基于势流理论的三维面元法,对三体船的斜拖运动进行数值模拟,并求得相应的水动力系数。将传统的运用于机翼升力计算的涡环栅格法(VLM)运用于三体船斜拖运动的数值模拟,船体表面被离散成四边形的网格,网格及尾涡面上布置一个涡环,利用船体表面不可穿透条件以及尾缘处的库塔条件对各单元涡强进行求解,求得各个分布点压强以及船体表面压力分布,并根据压力分布积分求得在不同漂角下三体船舶所受的横向力以及转首力矩。最终由计算结果,求得与漂角相关的水动力系数,并与软件计算结果进行对比分析。 展开更多
关键词 三体船 操纵性 栅格 横向力 转首力矩
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三维机翼尾涡面卷曲的数值模拟 被引量:1
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作者 谭廷寿 张元坤 《武汉理工大学学报(交通科学与工程版)》 2005年第6期844-847,共4页
采用离散涡环法来模拟三维机翼的升力效应,机翼尾涡面由双曲四边形面元进行离散,每个面元上布置线性偶极子分布,由尾涡面上的运动学条件来确定三维涡面卷曲形状,在诱导速度计算中引入了非奇异化的光滑参数,数值模拟结果显示了本方法的... 采用离散涡环法来模拟三维机翼的升力效应,机翼尾涡面由双曲四边形面元进行离散,每个面元上布置线性偶极子分布,由尾涡面上的运动学条件来确定三维涡面卷曲形状,在诱导速度计算中引入了非奇异化的光滑参数,数值模拟结果显示了本方法的有效性,与试验结果和其他数值方法相比是吻合的. 展开更多
关键词 机翼 面卷曲 涡环法
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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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Multi-criteria assessment of offshore wind turbine support structures based on dynamic property optimization
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作者 孟珣 Shi Ruifeng 《High Technology Letters》 EI CAS 2014年第4期421-428,共8页
Increasing size of wind turbine and deep water deployment have raised the issue of appropriate selection of the most suitable support structure to make offshore wind energy cost competitive.The paper presents an optim... Increasing size of wind turbine and deep water deployment have raised the issue of appropriate selection of the most suitable support structure to make offshore wind energy cost competitive.The paper presents an optimization methodology for decision making process of bottom mounted supports of offshore wind turbines (OWTs) through reasonable engineering attributes derivation.Mathematic models of support structures are reduced by the generalized single-degree-of-freedom theory with relatively fewer structural parameters.Soft-stiff design optimization based on dynamic properties of OWTs is performed for monopile and lattice supports with different wind turbines,water depth and hub height.Attributes of support structures,wind turbines and environment conditions are applied in the multi-criteria decision making method——TOPSIS for benchmarking of those options.The results illustrate the effectiveness of the proposed optimazation methodology combined with economical and environmental attributes together. 展开更多
关键词 offshore wind turbines (OWTs) support structure finite element method generalized single-degree-of-freedom (GSDOF) system dynamic property technique for order preference by similarity to ideal solution (TOPSIS) method
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