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二维结构/非结构混合网格的生成及其流场模拟 被引量:4
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作者 王平 朱自强 +1 位作者 拓双芬 尹幸愉 《航空学报》 EI CAS CSCD 北大核心 2001年第6期536-538,共3页
采用分区求解方法在二维结构 /非结构混合网格中对粘性绕流作了数值模拟。利用层面推进法生成绕物体的 O形结构网格 ,利用推进阵面法在结构网格外生成非结构网格。在结构网格区内 ,采用 B-L湍流模型 ,求解雷诺平均 N-S方程。在非结构网... 采用分区求解方法在二维结构 /非结构混合网格中对粘性绕流作了数值模拟。利用层面推进法生成绕物体的 O形结构网格 ,利用推进阵面法在结构网格外生成非结构网格。在结构网格区内 ,采用 B-L湍流模型 ,求解雷诺平均 N-S方程。在非结构网格区内求解 Euler方程。两区的解通过在交界面上满足通量守恒条件进行耦合。 展开更多
关键词 结构/结构混合网格 分区求解方法 粘性流动 数值模拟 层面推进法 推进阵面法 雷诺平均N-S方程
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国家数值风洞风雷软件结构/非结构混合网格同构计算特性
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作者 杜一鸣 麻彤 +1 位作者 邱福生 陈祖昌 《气动研究与试验》 2024年第5期22-39,共18页
传统计算流体力学(CFD)结构与非结构网格在网格生成难度、近壁区网格质量、远场网格密度等方面均具有互补性,若能够将两者结合构造“结构/非结构混合网格”,便可充分发挥不同网格类型的优势。基于国家数值风洞风雷软件的任意网格“同构... 传统计算流体力学(CFD)结构与非结构网格在网格生成难度、近壁区网格质量、远场网格密度等方面均具有互补性,若能够将两者结合构造“结构/非结构混合网格”,便可充分发挥不同网格类型的优势。基于国家数值风洞风雷软件的任意网格“同构混合计算”框架,采用RAE2822翼型和ONERA M6机翼标模算例,以日常生成习惯并保证网格规模相近的情况下,构造了结构、非结构以及结构/非结构混合网格,对比分析了不同类型网格的求解特性。初步研究结果表明,对于跨声速激波弱分离流动问题,采用风雷软件求解结构/非结构混合网格能够得到与实验数据吻合较好的计算结果,同时收敛性和计算效率较纯结构和非结构网格也更好。但结构-非结构计算域交界面处存在变量的不连续,近壁区结构网格的层数会对计算结果产生明显影响,只有保证足够的结构网格覆盖范围以及较好的过渡性才能保证近壁区求解精度。此外,根据计算经验提出了结构/非结构混合网格的生成策略和调用风雷软件进行计算的应用指南,能够为风雷软件工程应用提供参考。 展开更多
关键词 国家数值风洞风雷软件 结构/结构混合网格 气动标模验证 计算精度和效率 收敛性 工程应用指南
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应用混合网格分析复杂积冰翼型气动性能 被引量:5
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作者 陈科 曹义华 +1 位作者 安克文 李栋 《航空学报》 EI CAS CSCD 北大核心 2007年第B08期87-91,共5页
通过发展一种点-点对接的结构/非结构混合网格生成方法,避免了复杂积冰外形难以划分结构化网格的问题,并对复杂积冰翼型的气动性能进行了分析计算。在靠近积冰边界的内层采用了非结构网格以拟合复杂的边界,在非结构网格外采用结构化网... 通过发展一种点-点对接的结构/非结构混合网格生成方法,避免了复杂积冰外形难以划分结构化网格的问题,并对复杂积冰翼型的气动性能进行了分析计算。在靠近积冰边界的内层采用了非结构网格以拟合复杂的边界,在非结构网格外采用结构化网格以节省存储空间和计算时间。为了检验网格对选用湍流模型的影响,整个流动区域分别采用SST和SA湍流模型,求解了雷诺平均N-S方程。数值计算结果表明SST模型更适于模拟复杂分离流动,积冰对翼型的气动性能造成了严重的影响。 展开更多
关键词 结构/结构混合网格 网格生成 积冰 气动性能 湍流模型 计算流体力学
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弹性机翼跨音速静气动弹性问题研究 被引量:7
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作者 史爱明 杨永年 王刚 《工程力学》 EI CSCD 北大核心 2006年第5期173-176,共4页
在非结构网格基础上,采用有限体积法求解了Euler方程;在结构网格基础上,采用有限差分方法求解了N-S方程。同时采用结构影响系数法计及机翼结构系统的弹性影响,计算了弹性机翼的结构变形和气动力载荷。计算结果表明:后掠机翼结构系统的... 在非结构网格基础上,采用有限体积法求解了Euler方程;在结构网格基础上,采用有限差分方法求解了N-S方程。同时采用结构影响系数法计及机翼结构系统的弹性影响,计算了弹性机翼的结构变形和气动力载荷。计算结果表明:后掠机翼结构系统的弹性使弹性机翼产生了正的挠度和负的剖面扭转角;负的扭转角使弹性机翼的有效迎角减小;有效迎角的减小又使得弹性机翼的有效气动力载荷减小。针对算例机翼结构系统的弹性使弹性机翼的升力相对刚性机翼的升力减小27.9%。 展开更多
关键词 结构/非结构网格 EULER/N-S方程 结构影响系数法 弹性机翼 气动力载荷
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复杂积冰翼型气动性能分析 被引量:6
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作者 陈科 曹义华 +1 位作者 安克文 李栋 《航空动力学报》 EI CAS CSCD 北大核心 2007年第6期986-990,共5页
为了克服复杂外形难以划分结构化网格的问题,采用结构/非结构混合多块网格对复杂积冰翼型的气动性能-进行了分析计算.在靠近积冰边界的内层采用了非结构网格,在非结构网格外采用结构化网格以节省存储空间和计算时间.不同类型网格之间采... 为了克服复杂外形难以划分结构化网格的问题,采用结构/非结构混合多块网格对复杂积冰翼型的气动性能-进行了分析计算.在靠近积冰边界的内层采用了非结构网格,在非结构网格外采用结构化网格以节省存储空间和计算时间.不同类型网格之间采用了点点对接的方式以简化通量重构的处理方式.整个流动区域采用SST湍流模型,求解了雷诺平均N-S方程.数值计算结果表明结构/非结构混合多块网格在复杂积冰翼型气动性能计算上的可行性,积冰对翼型的气动性能造成了严重的影响. 展开更多
关键词 航空 航天推进系统 结构/结构混合网格 积冰 气动性能 计算流体力学
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Unstructured Grid Immersed Boundary Method for Numerical Simulation of Fluid Structure Interaction 被引量:2
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作者 明平剑 孙扬哲 +1 位作者 段文洋 张文平 《Journal of Marine Science and Application》 2010年第2期181-186,共6页
This paper presents an improved unstructured grid immersed boundary method.The advantages of both immersed boundary method and body fitted grids which are generated by unstructured grid technology are used to enhance ... This paper presents an improved unstructured grid immersed boundary method.The advantages of both immersed boundary method and body fitted grids which are generated by unstructured grid technology are used to enhance the computation efficiency of fluid structure interaction in complex domain.The Navier-Stokes equation was discretized spacially with collocated finite volume method and Euler implicit method in time domain.The rigid body motion was simulated by immersed boundary method in which the fluid and rigid body interface interaction was dealt with VOS(volume of solid) method.A new VOS calculation method based on graph was presented in which both immersed boundary points and cross points were collected in arbitrary order to form a graph.The method is verified with flow past oscillating cylinder. 展开更多
关键词 fluid structure interaction immersed boundary method VOS unstructured grids finite volume method
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A FVCOM-Based Unstructured Grid Wave, Current,Sediment Transport Model,I.Model Description and Validation 被引量:16
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作者 WU Lunyu CHEN Changsheng +3 位作者 GUO Peifang SHI Maochong QI Jianhua GE Jianzhong 《Journal of Ocean University of China》 SCIE CAS 2011年第1期1-8,共8页
An effort was made to couple FVCOM (a three-dimensional (3D),unstructured grid,Finite Volume Coastal Ocean Model) and FVCOM-SWAVE (an unstructured grid,finite-volume surface wave model) for the study of nearshore ocea... An effort was made to couple FVCOM (a three-dimensional (3D),unstructured grid,Finite Volume Coastal Ocean Model) and FVCOM-SWAVE (an unstructured grid,finite-volume surface wave model) for the study of nearshore ocean processes such as tides,circulation,storm surge,waves,sediment transport,and morphological evolution.The coupling between FVCOM and FVCOM-SWAVE was achieved through incorporating 3D radiation stress,wave-current-sediment-related bottom boundary layer,sea surface stress parameterizations,and morphology process.FVCOM also includes a 3D sediment transport module.With accurate fitting of irregular coastlines,the model provides a unique tool to study sediment dynamics in coastal ocean,estuaries,and wetlands where local geometries are characterized by inlets,islands,and intertidal marsh zones.The model was validated by two standard benchmark tests: 1) spectral waves approaching a mild sloping beach and 2) morphological changes of seabed in an idealized tidal inlet.In Test 1,model results were compared with both analytical solutions and laboratory experiments.A further comparison was also made with the structured grid Regional Ocean Model System (ROMS),which provides an insight into the performance of the two models with the same open boundary forcing. 展开更多
关键词 FVCOM COUPLING radiation stress wave-current-sediment-related bottom boundary layer MORPHOLOGY
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Unsteady analysis of six-DOF motion of a 6:1 prolate spheroid in viscous fluid
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作者 Ying Xiong Ying Xiong +1 位作者 Hui Guan ChuiJie Wu 《Science China(Physics,Mechanics & Astronomy)》 SCIE EI CAS CSCD 2017年第11期24-40,共17页
Free-moving simulations of airplanes, submarines and other automobiles under extreme and emergency conditions are becoming increasingly important from operational and tactical perspectives. Such simulations are fairly... Free-moving simulations of airplanes, submarines and other automobiles under extreme and emergency conditions are becoming increasingly important from operational and tactical perspectives. Such simulations are fairly challenging due to the extreme unsteady motions and high Re(Reynolds) numbers. The aim of this study is to perform a six-DOF motion simulation of a 6:1prolate spheroid that is falling in a fluid field. Prior to conducting the six-DOF simulation, some verification simulations were performed. First, a laminar flow past an inclined prolate spheroid at a Re number of 1000 and incidence angle of 45. with a tetrahedral mesh was simulated to verify the relevant targeted discrete method for an unstructured mesh. Second, to verify the LES(large eddy simulation) models and dependent parameters for the DDES(delayed detached eddy simulation), a turbulent flow past a sphere was performed at a subcritical Re number of 10000. Third, a steady maneuvering problem about a prolate spheroid pitching up from 0. to 30. incidence at a uniform angular velocity was established based on a dynamic tetrahedral mesh with changing topology and the ALE(arbitrary Lagrangian-Eulerian) method of fluid-structure coupling at a Re number of 4.2 × 10~6.Finally, two six-DOF motions of an inclined 6:1 prolate spheroid at an initial incidence of 45. were simulated at different Re numbers of 10000 and 4.2 × 10~6. 展开更多
关键词 unsteady six-DOF tetrahedral dynamic mesh discrete method DDES
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