期刊文献+
共找到342篇文章
< 1 2 18 >
每页显示 20 50 100
三维复杂界面非结构网格N-S/DSMC耦合方法
1
作者 陈飞同 王学德 《航空动力学报》 北大核心 2025年第9期149-157,共9页
针对近连续流过渡区多尺度绕流问题,学界发展了N-S(Navier-Stokes)/DSMC(direct simulation Monte Carlo)耦合方法,大多数此类求解器面临着耦合界面波动失稳的难题,因此对复杂外形和耦合界面的通用性值得重点研究。鉴于非结构网格面向... 针对近连续流过渡区多尺度绕流问题,学界发展了N-S(Navier-Stokes)/DSMC(direct simulation Monte Carlo)耦合方法,大多数此类求解器面临着耦合界面波动失稳的难题,因此对复杂外形和耦合界面的通用性值得重点研究。鉴于非结构网格面向复杂外形高度的贴体性、优良适应性以及工程领域对过渡流区高效通用型计算方法的需求,提出并实现了一套三维复杂界面四面体非结构网格N-S/DSMC耦合方法用于模拟高超声速过渡流。该方法使用局部克努森数作为连续失效参数划分连续/稀薄区域,并生成三维复杂N-S/DSMC耦合界面,沿分界面两侧分别推进一层或多层界面信息传递单元,基于边界状态法进行信息耦合。该耦合方法无需对复杂不规则分界面作光滑和修型处理,具备对复杂过渡流区工程问题数值模拟的通用性。分别对三维高超声速圆球和钝锥绕流进行模拟,数值结果显示:与参考文献中的DSMC方法相比,激波处数值和壁面特征值基本一致,最大误差不超过8%,但计算效率分别提高了1.74倍和2.28倍,验证了该耦合方法的正确性和高效性。 展开更多
关键词 n-s/DsMC耦合方法 四面体非结构网格 高超声速流 过渡流区 复杂界面耦合方法
原文传递
An h-adaptive Discontinuous Galerkin Method for Laminar Compressible Navier-Stokes Equations on Curved Mesh 被引量:3
2
作者 Sun Qiang L yu Hongqiang Wu Yizhao 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2016年第5期566-575,共10页
An h-adaptive method is developed for high-order discontinuous Galerkin methods(DGM)to solve the laminar compressible Navier-Stokes(N-S)equations on unstructured mesh.The vorticity is regarded as the indicator of adap... An h-adaptive method is developed for high-order discontinuous Galerkin methods(DGM)to solve the laminar compressible Navier-Stokes(N-S)equations on unstructured mesh.The vorticity is regarded as the indicator of adaptivity.The elements where the vorticity is larger than a pre-defined upper limit are refined,and those where the vorticity is smaller than a pre-defined lower limit are coarsened if they have been refined.A high-order geometric approximation of curved boundaries is adopted to ensure the accuracy.Numerical results indicate that highly accurate numerical results can be obtained with the adaptive method at relatively low expense. 展开更多
关键词 h-adaptivity high-order discontinuous Galerkin methods(DGM) n-s equations high-order boundary approximation
在线阅读 下载PDF
Application of Mixed Differential Quadrature Method for Solving the Coupled Two-Dimensional Incompressible Navier-Stokes Equation and Heat Equation 被引量:2
3
作者 A.S.J.AL-SAIF 朱正佑 《Journal of Shanghai University(English Edition)》 CAS 2003年第4期343-351,共9页
The traditional differential quadrature method was improved by using theupwind difference scheme for the convective terms to solve the coupled two-dimensionalincompressible Navier-stokes equations and heat equation. T... The traditional differential quadrature method was improved by using theupwind difference scheme for the convective terms to solve the coupled two-dimensionalincompressible Navier-stokes equations and heat equation. The new method was compared with theconventional differential quadrature method in the aspects of convergence and accuracy. The resultsshow that the new method is more accurate, and has better convergence than the conventionaldifferential quadrature method for numerically computing the steady-state solution. 展开更多
关键词 coupled n-s equation and heat equation differential quadrature method upwind difference scheme
在线阅读 下载PDF
The Coupled CFD/Free-Wake Method for Numerical Prediction of Rotor BVI Noise
4
作者 Wang Fei Xu Guohua Hu Zhiyuan 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2018年第5期800-811,共12页
A coupled Navier-Stokes/free-wake method is developed to predict the rotor aerodynamics and wake.The widely-used Farassat 1 Aformulation is adopted to predict the rotor noise.In the coupled method,the Reynolds-average... A coupled Navier-Stokes/free-wake method is developed to predict the rotor aerodynamics and wake.The widely-used Farassat 1 Aformulation is adopted to predict the rotor noise.In the coupled method,the Reynolds-averaged Navier-Stokes(RANS)solver is established to simulate complex aerodynamic phenomena around blade and the tip-wake is captured by a free-wake model without numerical dissipation in the off-body wake zone.To overcome the time-consuming of the coupling strategy in previous studies,a more efficient coupling strategy is presented,by which only the induced velocity on the outer boundary grid need to be calculated.In order to obtain blade control settings,a delta trimming procedure is developed,which is more efficient than traditional trim method in the calculation of Jacobian matrix.Several flight conditions are simulated to demonstrate the validity of the coupled method.Then the rotor noise of operational load survey(OLS)is studied by the developed method as an application and the computational results are shown to be in good agreements with the available experimental data. 展开更多
关键词 HELICOPTER ROTOR coupled n-s/free-wake method delta trim method BVI noise
在线阅读 下载PDF
A FINITE ELEMENT ADAPTIVE METHOD FOR SOLVING GENERALIZED STOKES PROSLEM
5
作者 D. A.Fokin Yang Zuosheng(Department of Aerodynamics ,NUAA 29 Yudao Street.Nanjing 21001 P.China) 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI 1994年第1期1-6,共6页
A stabilized and convergent finite element formulation for the generalized Stokes problem is proposed and a posteriori analysis is performed to produce an error indicator. On this basis adaptive numerical method for s... A stabilized and convergent finite element formulation for the generalized Stokes problem is proposed and a posteriori analysis is performed to produce an error indicator. On this basis adaptive numerical method for solying the problem is developed . Numerical calculations are performed to confirm the reliability and effectiveness of the method. 展开更多
关键词 FInITE ELEMEnT method error EsTIMATE n-s e-quation generalized sTOKEs problems adaptive FInITE ELEMEnT methods
在线阅读 下载PDF
The Effect of Tool Construction and Cutting Parameters on Surface Roughness and Vibration in Turning of AISI 1045 Steel Using Taguchi Method
6
作者 Rogov Vladimir Aleksandrovich Ghorbani Siamak 《Modern Mechanical Engineering》 2014年第1期8-18,共11页
This paper presents an experimental investigation focused on identifying the effects of cutting conditions and tool construction on the surface roughness and natural frequency in turning of AISI1045 steel. Machining e... This paper presents an experimental investigation focused on identifying the effects of cutting conditions and tool construction on the surface roughness and natural frequency in turning of AISI1045 steel. Machining experiments were carried out at the lathe using carbide cutting insert coated with TiC and two forms of cutting tools made of AISI 5140 steel. Three levels for spindle speed, depth of cut, feed rate and tool overhang were chosen as cutting variables. The Taguchi method L9 orthogonal array was applied to design of experiment. By the help of signal-to-noise ratio and analysis of variance, it was concluded that spindle speed has the significant effect on the surface roughness, while tool overhang is the dominant factor affecting natural frequency for both cutting tools. In addition, the optimum cutting conditions for surface roughness and natural frequency were found at different levels. Finally, confirmation experiments were conducted to verify the effectiveness and efficiency of the Taguchi method in optimizing the cutting parameters for surface roughness and natural frequency. 展开更多
关键词 surface ROUGHnEss Cutting Condition natural Frequency VIBRATIOn TURnInG AnOVA Taguchi method s/n Ratio
暂未订购
SERIES PERTURBATIONS APPROXIMATE SOLUTIONS TO N-S EQUATIONS AND MODIFICATION TO ASYMPTOTIC EXPANSION MATCHED METHOD
7
作者 李大鸣 张红萍 高永祥 《Applied Mathematics and Mechanics(English Edition)》 SCIE EI 2002年第8期963-972,共10页
A method that series perturbations approximate solutions to N-S equations with boundary conditions was discussed and adopted. Then the method was proved in which the asymptotic solutions of viscous fluid flow past a s... A method that series perturbations approximate solutions to N-S equations with boundary conditions was discussed and adopted. Then the method was proved in which the asymptotic solutions of viscous fluid flow past a sphere were deducted. By the ameliorative asymptotic expansion matched method, the matched functions, are determined easily and the ameliorative curve of drag coefficient is coincident well with measured data in the case that Reynolds number is less than or equal to 40 000. 展开更多
关键词 asymptotic expansion matched method series perturbation n-s equation viscous fluid flow past a sphere
在线阅读 下载PDF
Numerical Simulation of Boundary Layer with Spectral Method
8
作者 Zhiyong Liang Lewen Zhang Xianfu Wang(Wuhan Transportation University,Wuhan 430063, P.R.China) 《武汉理工大学学报(交通科学与工程版)》 1999年第S1期64-67,共4页
It is important to improve the speed of a ship,the friction resistance can be reduced by injection air at the bottom of a ship when the ship is running on the water.As the first part of the studying project,here numer... It is important to improve the speed of a ship,the friction resistance can be reduced by injection air at the bottom of a ship when the ship is running on the water.As the first part of the studying project,here numerical simulation study method,boundary condition and governing equations are presented.It is easy to study complicated problems from simple conditions,so the program concerning boundary layer condition is compiled to solve the problem.Here the spectral method is introduced,and the results are tested by Dorod’s results. 展开更多
关键词 micro BUBBLEs resistance reduction n s EQUATIOn numerical simulation BOUnDARY layer sPECTRAL method
在线阅读 下载PDF
Least Square Finite Element Method for Viscous Splitting of Unsteady Incompressible Navier–Stokes Equations
9
作者 SHUI Qing-xiang WANG Da-guo +1 位作者 HE Zhi-liang HUANG Jin 《China Ocean Engineering》 SCIE EI CSCD 2018年第4期490-500,共11页
In order to solve unsteady incompressible Navier–Stokes(N–S) equations, a new stabilized finite element method,called the viscous-splitting least square FEM, is proposed. In the model, the N–S equations are split i... In order to solve unsteady incompressible Navier–Stokes(N–S) equations, a new stabilized finite element method,called the viscous-splitting least square FEM, is proposed. In the model, the N–S equations are split into diffusive and convective parts in each time step. The diffusive part is discretized by the backward difference method in time and discretized by the standard Galerkin method in space. The convective part is a first-order nonlinear equation.After the linearization of the nonlinear part by Newton’s method, the convective part is also discretized by the backward difference method in time and discretized by least square scheme in space. C0-type element can be used for interpolation of the velocity and pressure in the present model. Driven cavity flow and flow past a circular cylinder are conducted to validate the present model. Numerical results agree with previous numerical results, and the model has high accuracy and can be used to simulate problems with complex geometry. 展开更多
关键词 unsteady incompressible ns equations viscous splitting newton's method least square finite element method driven cavity flow flow past a circular cylinder
在线阅读 下载PDF
CFD-Based Load Calculation Method for Monopile Support Configuration of Offshore Wind Turbine
10
作者 Guo Tongqing Tong Xiaolong Lu Zhiliang 《Transactions of Nanjing University of Aeronautics and Astronautics》 EI CSCD 2016年第1期88-94,共7页
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 in... 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. 展开更多
关键词 monopile-supported offshore wind turbine navier-stokes(n-s)equations volume of fluid(VOF) method small amplitude wave unsteady load
在线阅读 下载PDF
基于疲劳强度衰减模型的S-N曲线测定方法 被引量:11
11
作者 卢曦 郑松林 褚超美 《农业机械学报》 EI CAS CSCD 北大核心 2007年第7期152-155,共4页
基于经验的疲劳强度衰减模型,提出了一种测定材料和结构的S-N曲线简易方法,同时可以确定材料和结构的临界载荷。该方法通过单点应力下的疲劳试验和静强度测定,可以获得原来至少需要两级应力试验才能得到的材料和结构的疲劳曲线。用不同... 基于经验的疲劳强度衰减模型,提出了一种测定材料和结构的S-N曲线简易方法,同时可以确定材料和结构的临界载荷。该方法通过单点应力下的疲劳试验和静强度测定,可以获得原来至少需要两级应力试验才能得到的材料和结构的疲劳曲线。用不同材料的疲劳试验进行了S-N曲线测定和验证,结果表明,该方法能够准确而且快捷地测定S-N曲线和临界载荷,减少了疲劳试验费用和试验工作量。 展开更多
关键词 s-n曲线 测定方法 疲劳强度 衰减模型
在线阅读 下载PDF
基于主S-N曲线法的地铁车体焊缝疲劳分析 被引量:14
12
作者 岳译新 刘永强 李晓峰 《机车电传动》 北大核心 2012年第5期79-81,共3页
建立了包括焊缝在内的某B型地铁铝合金车体的有限元模型,采用美国ASME标准中"网格不敏感的结构应力法及主S-N曲线法",对车体焊缝进行了有限元分析,分析计算了焊缝上的应力集中以及焊缝的疲劳寿命与损伤。计算结果表明,所有焊... 建立了包括焊缝在内的某B型地铁铝合金车体的有限元模型,采用美国ASME标准中"网格不敏感的结构应力法及主S-N曲线法",对车体焊缝进行了有限元分析,分析计算了焊缝上的应力集中以及焊缝的疲劳寿命与损伤。计算结果表明,所有焊缝的疲劳寿命均达到了车体的设计寿命要求。 展开更多
关键词 铝合金车体 s-n曲线法 结构应力 焊缝疲劳 AsME标准
在线阅读 下载PDF
定量热像法预测焊接接头的S-N曲线和残余寿命 被引量:19
13
作者 樊俊铃 郭杏林 +1 位作者 赵延广 吴承伟 《材料工程》 EI CAS CSCD 北大核心 2011年第12期29-33,共5页
在恒定的平均应力作用下,考虑焊接接头的实际工况,利用红外热像技术建立了快速预测焊接接头疲劳参数和残余寿命的模型,实现了定量热像法对非均质焊接接头疲劳性能的评估。通过红外热像仪监测焊接接头表面局部热点的变化,定性分析了损伤... 在恒定的平均应力作用下,考虑焊接接头的实际工况,利用红外热像技术建立了快速预测焊接接头疲劳参数和残余寿命的模型,实现了定量热像法对非均质焊接接头疲劳性能的评估。通过红外热像仪监测焊接接头表面局部热点的变化,定性分析了损伤演化状态。结果表明:定量热像法克服了传统疲劳实验方法的局限性,可快速、准确地确定非均质焊接接头的疲劳性能。同时,通过对疲劳损伤过程中热点区域的实时监测说明其是一种有效的检测方法。 展开更多
关键词 定量热像法 s-n曲线 十字焊接接头 损伤累积 残余寿命
在线阅读 下载PDF
船体结构S-N曲线选取方法 被引量:7
14
作者 陈崧 竺一峰 +1 位作者 胡嘉骏 祁恩荣 《舰船科学技术》 北大核心 2014年第1期22-26,共5页
疲劳失效是船体结构破坏的主要模式之一。可采用S-N曲线法计算船体结构的疲劳寿命,S-N曲线的选取是该方法的关键内容之一。由于实际应用中可供选择的S-N曲线有限,无法全面涵盖所有类型的节点,规范中S-N曲线对于新型节点形式的适用性有... 疲劳失效是船体结构破坏的主要模式之一。可采用S-N曲线法计算船体结构的疲劳寿命,S-N曲线的选取是该方法的关键内容之一。由于实际应用中可供选择的S-N曲线有限,无法全面涵盖所有类型的节点,规范中S-N曲线对于新型节点形式的适用性有待进一步研究。本文对S-N曲线的类型因子进行研究,提出采用热点应力集中系数选取S-N曲线的一般原则。并计算2种典型节点的应力集中系数,将其与规范值进行比较,发现计算值普遍小于规范值,按规范计算所得的疲劳寿命将趋于保守。 展开更多
关键词 船体结构 s-n曲线 选取方法
在线阅读 下载PDF
解耦N-S/DSMC方法计算推力器真空羽流的边界条件研究 被引量:7
15
作者 唐振宇 贺碧蛟 蔡国飙 《推进技术》 EI CAS CSCD 北大核心 2014年第7期897-904,共8页
准确模拟羽流流场是合理评估空间推力器真空羽流效应的基础。因羽流流场同时包含连续和稀薄两种流动机理,通常采用解耦方式的Navier-Stokes(N-S)方程和直接模拟蒙特卡罗(DSMC)混合方法对其进行模拟。为保证解耦N-S/DSMC方法应用于羽流... 准确模拟羽流流场是合理评估空间推力器真空羽流效应的基础。因羽流流场同时包含连续和稀薄两种流动机理,通常采用解耦方式的Navier-Stokes(N-S)方程和直接模拟蒙特卡罗(DSMC)混合方法对其进行模拟。为保证解耦N-S/DSMC方法应用于羽流计算时的准确性并尽量提高其计算效率,对计算中的DSMC入口和喷管壁面等边界条件设置问题开展了研究。通过与文献中低总压工况的羽流试验数据比较,确定了合理设置DSMC入口边界位置、壁面反射类型、壁温等边界条件的方法。针对将此方法应用于实际推力器工况计算时效率过低的问题,通过多种数值试验,表明从喷管出口处开始沿KnGL为0.05的等值线作为DSMC入口界面可同时保证仿真精度和较高的计算效率;并证明实际工况下壁温设置对羽流场仿真结果影响不大。 展开更多
关键词 解耦n-s/DsMC方法 推力器真空羽流 边界条件 DsMC方法
原文传递
基于N-S方程的航行船舶辐射问题数值模拟 被引量:6
16
作者 吴乘胜 朱德祥 顾民 《船舶力学》 EI 北大核心 2008年第4期560-567,共8页
基于N-S(Navier-Stokes)方程,进行了航行船舶辐射问题的数值模拟,包括强制垂荡和强制纵摇的模拟,计算了船舶垂荡和纵摇的附加质量和阻尼。数值模拟中,控制方程—RANS(Reynolds Averaged Navier-Stokes)方程和连续性方程使用有限体积法离... 基于N-S(Navier-Stokes)方程,进行了航行船舶辐射问题的数值模拟,包括强制垂荡和强制纵摇的模拟,计算了船舶垂荡和纵摇的附加质量和阻尼。数值模拟中,控制方程—RANS(Reynolds Averaged Navier-Stokes)方程和连续性方程使用有限体积法离散,非线性自由面采用VOF方法处理。文中给出了以不同航速前进的船舶强制垂荡和纵摇的力与力矩,以及船舶垂荡和纵摇的附加质量系数和阻尼系数,并与DUT(Delft University of Technology)的试验数据进行了比较,二者吻合良好。 展开更多
关键词 ns方程 VOF法 辐射问题 附加质量 阻尼
在线阅读 下载PDF
带副翼的翼身组合体绕流的Euler和N-S方程解 被引量:7
17
作者 陈泽民 李津 +1 位作者 朱自强 吴宗成 《计算物理》 CSCD 北大核心 2001年第4期372-376,共5页
将对接分区网格与分区求解算法结合 ,有效地求解了带副翼偏转的翼身组合体绕流的N S方程 .数值方法中选用VanLeer分裂格式离散无粘通量项 ,采用中心差分格式来离散粘性通量项 .分区交界面采用了一种满足通量守恒的内边界耦合条件 .数值... 将对接分区网格与分区求解算法结合 ,有效地求解了带副翼偏转的翼身组合体绕流的N S方程 .数值方法中选用VanLeer分裂格式离散无粘通量项 ,采用中心差分格式来离散粘性通量项 .分区交界面采用了一种满足通量守恒的内边界耦合条件 .数值算例表明该方法是求解带操纵面偏转的翼身组合体绕流的有效方法 . 展开更多
关键词 副翼 翼身组合体绕流 EULER方程 n-s方程 分区算法 操纵面偏转 中心差分格式 网格结构 飞机 气动力计算
在线阅读 下载PDF
估计三种常用疲劳应力-寿命模型P-S-N曲线的统一经典极大似然法 被引量:40
18
作者 赵永翔 王金诺 高庆 《应用力学学报》 EI CAS CSCD 北大核心 2001年第1期83-90,共8页
拓展经典极大似然法到Langer模型,提出了估计三参数、Langer和Basquin三种常用疲劳应力-寿命模型P-S-N曲线及其置信限的统一方法。方法用于处理极大似然法疲劳试验得到的S-N数据。该试验在特别关注的参考载荷试验一组试样,其余试样在... 拓展经典极大似然法到Langer模型,提出了估计三参数、Langer和Basquin三种常用疲劳应力-寿命模型P-S-N曲线及其置信限的统一方法。方法用于处理极大似然法疲劳试验得到的S-N数据。该试验在特别关注的参考载荷试验一组试样,其余试样在不同载荷下试验。以参考载荷试验数据的统计参量为基础,按照每个模型中材料常数协同处于相同概率水平原则,将曲线表示为对数疲劳寿命均值和均方差线的广义形式,至多4个材料常数。曲线中的材料常数按极大似然原理采用数学规划法求出。45#碳钢缺口试样(kt=20)对称循环加载试验数据的分析说明了方法的有效性。分析还揭示合理模型有必要通过比较拟合效果、预计误差和应用安全性来确定。三参数模型的拟合效果最好,Langer模型稍差,Basquin模型较差。从拟合效果、预计误差和应用安全性角度,Basquin模型不适于描述该套数据。此外,经典极大似然法估计结果可能因受局部统计参量影响而给出非安全估计,有必要发展改进的可以最大限度减小这种影响的方法。 展开更多
关键词 疲劳 应力-寿命模型 P-s-n曲线 经典极大似然法
在线阅读 下载PDF
跨声速机翼抖振初始迎角N-S方程定常计算分析 被引量:10
19
作者 郭同庆 董璐 陆志良 《航空学报》 EI CAS CSCD 北大核心 2008年第4期840-844,共5页
应用代数法和椭圆型方程优化相结合的方法生成翼身组合体块结构网格。采用有限体积空间离散法和五步Runge-Kutta显式时间推进法求解N-S方程。基于雷诺平均N-S(RANS)方程,选用Spalart-Allma-ras(SA)一方程模型模拟紊流。根据N-S方程定常... 应用代数法和椭圆型方程优化相结合的方法生成翼身组合体块结构网格。采用有限体积空间离散法和五步Runge-Kutta显式时间推进法求解N-S方程。基于雷诺平均N-S(RANS)方程,选用Spalart-Allma-ras(SA)一方程模型模拟紊流。根据N-S方程定常计算结果,采用升力曲线、俯仰力矩曲线、后缘压力发散、跨声速激波位置以及机翼表面极限流线等几种判据,对跨声速机翼的抖振初始迎角进行了合理的预测分析。 展开更多
关键词 块结构网格 有限体积法 n-s方程 紊流模型 抖振
在线阅读 下载PDF
带副翼三维机翼绕流的N-S方程解 被引量:4
20
作者 李津 朱自强 +1 位作者 陈泽民 李海明 《航空学报》 EI CAS CSCD 北大核心 1999年第3期197-200,共4页
提出了一种求解带副翼偏转三维机翼绕流的N-S方程计算方法。采用对接分区网格与分区求解算法的结合,有效地求解绕此外形的复杂流动。提出了一种满足通量守恒的内边界耦合条件。数值方法中选用vanLeer分裂格式离散无粘通量项... 提出了一种求解带副翼偏转三维机翼绕流的N-S方程计算方法。采用对接分区网格与分区求解算法的结合,有效地求解绕此外形的复杂流动。提出了一种满足通量守恒的内边界耦合条件。数值方法中选用vanLeer分裂格式离散无粘通量项,并构造了一种Limiter函数以保证TVD性质,采用中心差分格式来离散粘性通量项。数值算例表明该方法是求解带操纵面偏转的机翼绕流的有效方法。 展开更多
关键词 n-s方程 分区算法 机翼 副翼 三维 绕流
在线阅读 下载PDF
上一页 1 2 18 下一页 到第
使用帮助 返回顶部