ANSYS 官方帮助文件 05-udf

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ansys-中文帮助手册(含目录-word版本)

ansys-中文帮助手册(含目录-word版本)

ansys-中文帮助手册(含目录-word版本)目录第1 章开始使用ANSYS 11.1 完成典型的ANSYS 分析 1 1.2 建立模型 1第2 章加载232.1 载荷概述23 2.2 什么是载荷23 2.3 载荷步、子步和平衡迭代24 2.4 跟踪中时间的作用25 2.5 阶跃载荷与坡道载荷26 2.6 如何加载27 2.7 如何指定载荷步选项68 2.8 创建多载荷步文件77 2.9 定义接头固定处预拉伸78第3 章求解853.1 什么是求解84 3.2 选择求解器84 3.3 使用波前求解器85 3.4 使用稀疏阵直接解法求解器86 3.5 使用雅可比共轭梯度法求解器(JCG)86 3.6 使用不完全乔列斯基共轭梯度法求解器(ICCG)86 3.7 使用预条件共轭梯度法求解器(PCG)86 3.8 使用代数多栅求解器(AMG)87 3.9 使用分布式求解器(DDS)88 3.10 自动迭代(快速)求解器选项88 3.11 在某些类型结构分析使用特殊求解控制89 3.12 使用PGR 文件存储后处理数据92 3.13 获得解答96 3.14 求解多载荷步97 3.15 中断正在运行的作业100 3.16 重新启动一个分析100 3.17 实施部分求解步111 3.18 估计运行时间和文件大小1133.19 奇异解114第4 章后处理概述1164.1 什么是后处理116 4.2 结果文件117 4.3 后处理可用的数据类型117第5 章通用后处理器(POST1) 1185.1 概述118 5.2 将数据结果读入数据库118 5.3 在POST1 中观察结果127 5.4 在POST1 中使用PGR 文件152 5.5 POST1 的其他后处理内容160第6 章时间历程后处理器(POST26)1746.1 时间历程变量观察器174 6.2 进入时间历程处理器176 6.3 定义变量177 6.4 处理变量并进行计算179 6.5 数据的输入181 6.6 数据的输出183 6.7 变量的评价184 6.8 POST26 后处理器的其它功能187 第7 章选择和组件190 7.1 什么是选择190 7.2 选择实体190 7.3 为有意义的后处理选择194 7.4 将几何项目组集成部件与组件195 第8 章图形使用入门1988.1 概述198 8.2 交互式图形与“外部”图形198 8.3 标识图形设备名(UNIX 系统)198 8.4 指定图形显示设备的类型(WINDOWS 系统)2018.5 与系统相关的图形信息202 8.6 产生图形显示205 8.7 多重绘图技术207第9 章通用图形规范2109.1 概述210 9.2 用GUI 控制显示210 9.3 多个ANSYS 窗口,叠加显示210 9.4 改变观察角、缩放及平移211 9.5 控制各种文本和符号214 9.6 图形规范杂项217 9.7 3D 输入设备支持218第10 章增强型图形21910.1 图形显示的两种方法219 10.2P OWER G RAPHICS 的特性219 10.3何时用P OWER G RAPHICS219 10.4激活和关闭P OWER G RAPHICS220 10.5怎样使用P OWER G RAPHICS220 10.6希望从P OWER G RAPHICS 绘图中做什么220第11 章创建几何显示22311.1 用GUI 显示几何体223 11.2 创建实体模型实体的显示223 11.3 改变几何显示的说明224第12 章创建几何模型结果显示23312.1 利用GUI 来显示几何模型结果233 12.2 创建结果的几何显示233 12.3 改变POST1 结果显示规范235 12.4 Q-S LICE 技术238 12.5 等值面技术238 12.6 控制粒子流或带电粒子的轨迹显示239第13 章生成图形24013.1 使用GUI 生成及控制图240 13.2 图形显示动作240 13.3 改变图形显示指定241第14章注释24514.1 注释概述245 14.2 二维注释245 14.3 为ANSYS 模型生成注释246 14.4 三维注释246 14.5 三维查询注释247第15 章动画24815.1 动画概述248 15.2 在ANSYS 中生成动画显示248 15.3 使用基本的动画命令248 15.4 使用单步动画宏249 15.5 离线捕捉动画显示图形序列249 15.6 独立的动画程序250 15.7 WINDOWS 环境中的动画251第16 章外部图形25316.1 外部图形概述253 16.2 生成中性图形文件254 16.3 DISPLAY 程序观察及转换中性图形文件255 16.4 获得硬拷贝图形258 第17 章报告生成器25917.1 启动报告生成器259 17.2 抓取图象260 17.3 捕捉动画260 17.4 获得数据表格261 17.5 获取列表264 17.6 生成报告26417.7 报告生成器的默认设置267 第18 章 CMAP 程序26918.1 CMAP 概述269 18.2 作为独立程序启动CMAP269 18.3 在ANSYS 内部使用CMAP271 18.4 用户化彩色图271第19 章文件和文件管理27419.1 文件管理概述274 19.2 更改缺省文件名274 19.3 将输出送到屏幕、文件或屏幕及文件275 19.4 文本文件及二进制文件275 19.5 将自己的文件读入ANSYS 程序278 19.6 在ANSYS 程序中写自己的ANSYS 文件279 19.7 分配不同的文件名280 19.8 观察二进制文件内容(AXU2)280 19.9 在结果文件上的操作(AUX3)280 19.10 其它文件管理命令280第20 章内存管理与配置28220.1 内存管理282 20.2 基本概念282 20.3 怎样及何时进行内存管理283 20.4 配置文件286第1 章开始使用ANSYS1.1 完成典型的ANSYS 分析ANSYS 软件具有多种有限元分析的能力,包括从简单线性静态分析到复杂的非线性瞬态动力学分析。

ANSYS的帮助文件使用说明

ANSYS的帮助文件使用说明

ANSYS的帮助文件使用说明很多网友都曾觉得ANSYS使用起来有一定的难度,经常会遇到这样或那样的问题,但市面上的参考书又不尽如人意,那究竟有没有比较好的参数书?有的,个人认为ANSYS的帮助文件就是一本不错的参数书。

接下来就ANSYS在线帮助的使用做一些基本的介绍,希望能对初学者有所帮助。

ANSYS的帮助文件包括所有ANSYS命令解释及所有的GUI解释,还包括ANSYS各模块的分析指南,实例练习等。

一.进入帮助系统可以通过下列三种方式进入:1.进入ANSYS的操作界面后,在应用菜单中选取Help进入;2.在ANSYS程序组中选取Help System进入:Start Menu > Programs > ANSYS XX>Help Sy stem;3.在任何对话框中选取Help。

二.帮助系统的内容安排:点击帮助系统的目录,就看到如下的ANSYS帮助系统的整体内容安排:1.前面4个部分是与软件版本,安装,注册相关的信息,只需作相应的了解即可,如下:※Release Notes※ANSYS Installation and Configuration Guide for UNIX※ANSYS Installation and Configuration Guide for Windows※ANSYS, Inc. Licensing Guide2.接下来两个部分是比较重要的部分,ANSYS的命令和单元手册,对用到的命令和单元应作详细的了解和掌握。

※ANSYS Commands Reference※ANSYS Element Reference3.下面四个部分是ANSYS相关的操作手册,说明如下:※Operations Guide 基本界面,操作指南※Basic Analysis Procedures Guide 基础分析指南※Advanced Analysis Techniques Guide 高级分析指南※Modeling and Meshing Guide 建模与分网指南4.以下几个部分则是ANSYS分模块的分析指南,如下:※Structural Analysis Guide 结构分析指南※Thermal Analysis Guide 热分析指南※CFD FLOTRAN Analysis Guide 流体分析指南※Electromagnetic Field Analysis Guide 电磁场分析指南※Coupled-Field Analysis Guide 耦合场分析指南5.为更好的使用ANSYS方便,快捷的解决更多的工程实际问题,建议仔细学习以下几个部分:※APDL Programmer's Guide:APDL操作手册※ANSYS Troubleshooting Guide:ANSYS错误信息指南※Mechanical Toolbar:机械工具栏※ANSYS/LS-DYNA User's Guide:ANSYS/LS-DYNA操作指南※ANSYS Connection Users Guide:接口技术指南6.欲快速掌握ANSYS的使用,莫过于通过实例和练习,而ANSYS的帮助系统中则提供大量的例题及练习供用户参考,所以以下两个部分是经常光顾的。

Ansys Fluent 13.0 or 14.0 Tutorials教程

Ansys Fluent 13.0 or 14.0 Tutorials教程

Ansys FLUENT Tutorials└─ANSYS FLUENT├─ANSYS-FLUENT-Intro_13.0_1st-ed_pdf││fluent_13.0_Agenda.pdf││fluent_13.0_TOC.pdf│││├─lectures││fluent_13.0_lecture01-welcome.pdf││fluent_13.0_lecture02-intro-to-cfd.pdf││fluent_13.0_lecture03-solver-basics.pdf││fluent_13.0_lecture04-boundary-conditions.pdf ││fluent_13.0_lecture05-solver-settings.pdf││fluent_13.0_lecture06-turbulence.pdf││fluent_13.0_lecture07-heat-transfer.pdf││fluent_13.0_lecture08-udf.pdf││fluent_13.0_lecture09-physics.pdf││fluent_13.0_lecture10-transient.pdf││fluent_13.0_lecture11-post.pdf│││├─workshop-input-files││├─workshop1-mixing-tee│││ fluidtee.meshdat│││││├─workshop2-airfoil-new│││ NACA0012.msh│││ mach_0.5_comparison.cas.gz│││ mach_0.5_comparison.dat.gz│││ mach_0.7_converged.cas.gz│││ mach_0.7_converged.dat.gz│││ test-data-bottom.xy│││ test-data-top.xy│││││├─workshop3-multi-species│││ calc_activities.jou│││ garage.msh│││ workshop3-converged.cas.gz│││ workshop3-converged.dat.gz│││││├─workshop4-electronics│││ heatsink.msh.gz│││ ws4_no-radiation.cas.gz│││ ws4_no-radiation.dat.gz│││ ws4_s2s-radiation.cas.gz│││ ws4_s2s-radiation.dat.gz│││ ws4_viewfactor.s2s.gz│││││├─workshop5-moving-parts│││ ws5-mesh-animation.avi│││ ws5-simple-wind-turbine.msh│││ ws5_udf_for_motion.c│││││├─workshop6-dpm│││ dpm_tutorial.msh│││││└─workshop7-tank-flush││tankflush.msh.gz││ws7-tankflush-animation.avi││ws7-tankflush-animation.mpeg│││└─workshops│fluent_13.0_WS_TOC.pdf│fluent_13.0_workshop01-mixingtee.pdf│fluent_13.0_workshop02-airfoil.pdf│fluent_13.0_workshop03-Multiple-Species.pdf│fluent_13.0_workshop04-electronics.pdf│fluent_13.0_workshop05-moving-parts.pdf│fluent_13.0_workshop06-dpm.pdf│fluent_13.0_workshop07-tank-flush.pdf│├─Quick Tutorials││ FLUENT_Overview_1_Introduction_to_FLUENT12_in_ANSYS_Workbench_DOC.pd f││ FLUENT_Overview_1_Introduction_to_FLUENT12_in_ANSYS_Workbench_WA TCH ME.swf││ FLUENT_Overview_2_Creating_and_Comparing_Related_FLUENT12_Analyses_in_ ANSYS_Workbench_DOC.pdf││ FLUENT_Overview_2_Creating_and_Comparing_Related_FLUENT12_Analyses_in_ ANSYS_Workbench_WA TCHME.swf││ FLUENT_Overview_3_Parametric_Study_Using_FLUENT12_in_ANSYS_Workbench _DOC.pdf││ FLUENT_Overview_3_Parametric_Study_Using_FLUENT12_in_ANSYS_Workbench _WATCHME.swf││ FLUENT_Overview_4_1-Way_Fluid-Structure_Interaction_Using_FLUENT12_and_A NSYS_Mechanical_DOC.pdf││ FLUENT_Overview_4_1-Way_Fluid-Structure_Interaction_Using_FLUENT12_and_A NSYS_Mechanical_WA TCHME.swf│││├─FLUENT_Overview_1_FILES││ probe.agdb│││├─FLUENT_Overview_2_FILES│││ Duplicate_Probe_Fluent.wbpj│││││└─Duplicate_Probe_Fluent_files│││ .project_cache│││││├─dp0││││ designPoint.wbdp│││││││├─FFF││││├─DM│││││ FFF.agdb│││││││││├─Fluent│││││ FFF-1-00100.dat.gz│││││ FFF-1.cas.gz│││││ FFF.set│││││││││├─MECH│││││ FFF.msh│││││││││└─Post││││Probe.cst│││││││├─FFF-1││││└─Fluent││││FFF-1.1-1-00081.dat.gz │││││││└─global│││└─MECH││││ FFF.mshdb│││││││└─FFF││└─user_files│├─FLUENT_Overview_3_FILES│││ Parametric_Probe_Fluent.wbpj│││││└─Parametric_Probe_Fluent_files│││ .project_cache│││││├─dp0││││ designPoint.wbdp│││││││├─FFF││││├─DM│││││ FFF.agdb│││││││││├─Fluent│││││ FFF-1-00100.dat.gz│││││ FFF-1.cas.gz│││││ FFF.set│││││││││├─MECH│││││ FFF.msh│││││││││└─Post││││Probe.cst│││││││├─FFF-1││││└─Fluent││││FFF-1.1-1-00081.dat.gz │││││││└─global│││└─MECH││││ FFF.mshdb│││││││└─FFF││└─user_files│└─FLUENT_Overview_4_FILES││ FSI_Probe_Fluent.wbpj│││└─FSI_P robe_Fluent_files││ .project_cache│││├─dp0│││ designPoint.wbdp│││││├─FFF│││├─DM││││ FFF.agdb│││││││├─Fluent││││ FFF-1-00100.dat.gz││││ FFF-1.cas.gz││││ FFF.set│││││││├─MECH││││ FFF.msh│││││││└─Post│││Probe.cst│││││├─FFF-1│││└─Fluent│││FFF-1.1-1-00081.dat.gz│││││└─global││└─MECH│││ FFF.mshdb│││││└─FFF│└─user_files├─combustion-fluent││ combustion-tutorial-list_13.0.pdf││ tut-01-intro-tut-16-species-transport.pdf││ tut-02-intro-tut-17-non-premix-combustion.pdf ││ tut-03-intro-tut-18-surface-chemistry.pdf││ tut-04-intro-tut-19-evaporating-liquid.pdf││ tut-05-berl.pdf││ tut-06-finite-rate.pdf││ tut-07-pdf-jet.pdf││ tut-08-cijr.pdf││ tut-09-pilot-jet.pdf││ tut-10-zimont.pdf││ tut-11-surfchem.pdf││ tut-12-mchar.pdf││ tut-13-co-combustor.pdf││ tut-14-flamelet.pdf││ tut-15-moss-brookes.pdf││ tut-16-dqmom.pdf││ tut-17-species.pdf││ tut-18-euler-granular.pdf││ tut-19-dpm-channel.pdf│││├─tut-01-intro-tut-16-species-transport│││ gascomb.msh│││││└─solution_files││gascomb1.cas.gz││gascomb1.dat.gz││gascomb2.dat.gz││gascomb3.cas.gz││gascomb3.dat.gz│││├─tut-02-intro-tut-17-non-premix-combustion │││ berl.msh│││ berl.prof│││││└─solution_files││berl-1.cas.gz││berl-1.dat.gz││berl.pdf│││├─tut-03-intro-tut-18-surface-chemistry│││ surface.msh│││││└─solution_files││surface-non-react.cas.gz││surface-react1.cas.gz││surface-react1.dat.gz││surface-react2.cas.gz││surface-react2.dat.gz│││├─tut-04-intro-tut-19-evaporating-liquid│││ sector.msh│││││└─solution_files││sector.msh││spray1.cas.gz││spray1.dat.gz││spray2.cas.gz││spray2.dat.gz││spray3.cas.gz││spray3.dat.gz│││├─tut-05-berl│││ berl.msh.gz│││ berl.prof│││││└─solution_files││berl-mag-1.cas.gz││berl-mag-1.dat.gz││berl-mag-2.cas.gz││berl-mag-3.cas.gz ││berl-mag-3.dat.gz │││├─tut-06-finite-rate│││ conreac.msh.gz│││││└─solution_files││5step.cas.gz││5step.dat.gz││5step_cold.cas.gz ││5step_cold.dat.gz ││5step_final.cas.gz │││├─tut-07-pdf-jet│││ CH4-skel.che│││ flameD.msh.gz│││ therm.dat│││││└─solution_files││flameD-1.cas.gz ││flameD-1.dat.gz ││flameD-2.cas.gz ││flameD-2.dat.gz ││flameD-3.cas.gz ││flameD-3.dat.gz ││flameD.pdf.gz││surf-mon-1.out │││├─tut-08-cijr│││ CIJR-therm.dat│││ CIJR.che│││ CIJR.msh.gz│││││└─solution_files││CIJR-1.cas.gz││CIJR-1.dat.gz││CIJR-2.cas.gz││CIJR-2.dat.gz││CIJR-3.cas.gz││CIJR-3.dat.gz││CIJR-4.cas.gz││CIJR-4.dat.gz││CIJR-4.fla.gz││CIJR.fla.gz││CIJR.pdf.gz││CIJRdisplay.cas.gz ││CIJRdisplay.dat.gz │││├─tut-09-pilot-jet│││ flameD-sfla.msh.gz│││ gri30.che│││││└─solution_files││flameD-sfla-1.cas.gz ││flameD-sfla-1.dat.gz ││flameD-sfla.fla.gz ││flameD-sfla.pdf.gz ││flameD-ufla-1.cas.gz ││flameD-ufla-1.dat.gz ││flameD-ufla-1.fla.gz ││surf-mon-1.out│││├─tut-10-zimont│││ conreac.msh│││││└─solution_files││zimont-ad.cas.gz││zimont-ad.dat.gz││zimont-nonad.cas.gz ││zimont-nonad.dat.gz ││zimont.cas.gz│││├─tut-11-surfchem│││ gas_chem.che│││ surf_chem.che│││ test.msh.gz│││││└─solution_files││surf-cat-comb.cas.gz ││surf-cat-comb.dat.gz ││surf-mon-1.out│││├─tu t-12-mchar│││ mchar.msh.gz│││││└─solution_files││mchar-rad.cas.gz││mchar-rad.dat.gz││mchar.cas.gz││mchar.dat.gz││view-0.vw│││├─tut-13-co-combustor│││ par-premixed.msh.gz│││││└─solution_files││par-premixed.pdf.gz││peters-partially-premixed-2nd.cas.gz ││peters-partially-premixed-2nd.dat.gz ││zimont-partially-premixed-1st.cas.gz ││zimont-partially-premixed-1st.dat.gz ││zimont-partially-premixed-2nd.cas.gz ││zimont-partially-premixed-2nd.dat.gz ││zimont-partially-premixed.cas.gz││zimont-partially-premixed.dat.gz│││├─tut-14-flamelet│││ berl.msh.gz│││ berl.prof│││ smooke46.che│││ thermo.db│││││└─solution_files││berl-converged.cas.gz││berl-converged.dat.gz││berl-ini.cas.gz││berl-second.cas.gz││berl-second.dat.gz││berl.fla.gz││berl.pdf.gz│││├─tut-15-moss-brookes│││ brookes_ch4.cas.gz│││ brookes_ch4.dat.gz│││ brookes_ch4.pdf.gz│││ brookes_ch4.ray│││ flamlet.fla│││ therm.dat│││││└─solution_files││brookes_ch4_soot_converged.cas.gz││brookes_ch4_soot_converged.dat.gz │││├─tut-16-dqmom│││ dqmom.msh.gz│││││└─solution_files││dqmom-1.cas.gz││dqmom-1.dat.gz││dqmom-2.cas.gz││dqmom-2.dat.gz││dqmom-final.cas.gz││dqmom-final.dat.gz││dqmom-init.cas.gz││dqmom-init.dat.gz││dqmom.cas.gz││dqmom.dat.gz│││├─tut-17-species│││ baffled_reactor.msh.gz│││││└─solution_files││case-1-rtd-complete.cas.gz││case-1-rtd-complete.dat.gz││case-1-tracer-init.cas.gz││case-1-tracer-init.dat.gz││case-1-tracer-injection-complete.cas.gz ││case-1-tracer-injection-complete.dat.gz ││case-1-tracer.out││case-1.cas.gz││case-1.dat.gz││case-2-rtd-complete.cas.gz││case-2-rtd-complete.dat.gz││case-2-rtd-final.cas.gz││case-2-rtd-final.dat.gz││case-2-tracer-init.cas.gz││case-2-tracer-init.dat.gz││case-2-tracer-injection-complete.cas.gz ││case-2-tracer-injection-complete.dat.gz ││case-2-tracer.out││case-2.cas.gz││case-2.dat.gz││surf-mon-1.out│││├─tut-18-euler-granular│││ euler.msh.gz│││ mass_xfer_rate.c│││││└─solution_files││euler-gran-1.cas.gz││euler-gran-1.dat.gz││euler-gran-final.cas.gz││euler-gran-final.dat.gz││vol-solid.out│││└─tut-19-dpm-channel││ 3dpipe.msh.gz│││└─solution_files│ dpm-evap.cas.gz│ dpm-evap.dat.gz│ pipe-flow.cas.gz│ pipe-flow.dat.gz│├─extra││ FLUENT13_workshop_XX_RAE_Airfoil.pptx ││ FLUENT13_workshop_XX_V ortexShedding.pptx │││├─workshop_XX_RAE_Airfoil│││ ExperimentalData.csv│││ coarse.xy│││ experiment.xy│││ expressions.cst│││ rae2822_coarse.msh│││││└─Result_TUT_04│││ rae2822_coarse-data_export_to_post.cas │││ rae2822_coarse-data_export_to_post.cdat │││ rae2822_coarse-data_export_to_post.cst│││ rae2822_coarse.cas.gz│││ rae2822_coarse.dat.gz│││││└─FINE_MESH││ medium.xy││ rae2822_fine.cas.gz││ rae2822_fine.dat.gz││ rae2822_fine.msh││ rae2822_medium.cas.gz││ rae2822_medium.dat.gz││ rae2822_medium.msh│││└─workshop_XX_V ortexShedding││ point-4-y-velocity-final.out││ vortex-shedding-coarse.msh││ vortex-shedding-unsteady.cas.gz││ vortex-shedding-unsteady.dat.gz│││├─FILES_FOR_CFDPOST││ vectors.mp4││ vortex-shedding-unsteady-3-68.949997.dat.gz ││ vortex-shedding-unsteady-3-69.199997.dat.gz ││ vortex-shedding-unsteady-3-69.449997.dat.gz ││ vortex-shedding-unsteady-3-69.699997.dat.gz ││ vortex-shedding-unsteady-3-69.949997.dat.gz ││ vortex-shedding-unsteady-3-70.199997.dat.gz ││ vortex-shedding-unsteady-3-70.449997.dat.gz ││ vortex-shedding-unsteady-3-70.699997.dat.gz ││ vortex-shedding-unsteady-3-70.949997.dat.gz ││ vortex-shedding-unsteady-3-71.199997.dat.gz ││ vortex-shedding-unsteady-3-71.449997.dat.gz ││ vortex-shedding-unsteady-3-71.699997.dat.gz ││ vortex-shedding-unsteady-3-71.949997.dat.gz ││ vortex-shedding-unsteady-3-72.199997.dat.gz ││ vortex-shedding-unsteady-3-72.449997.dat.gz ││ vortex-shedding-unsteady-3-72.699997.dat.gz ││ vortex-shedding-unsteady-3-72.949997.dat.gz ││ vortex-shedding-unsteady-3-73.199997.dat.gz ││ vortex-shedding-unsteady-3-73.449997.dat.gz ││ vortex-shedding-unsteady-3-73.699997.dat.gz ││ vortex-shedding-unsteady-3-73.949997.dat.gz ││ vortex-shedding-unsteady-3-74.199997.dat.gz ││ vortex-shedding-unsteady-3-74.449997.dat.gz ││ vortex-shedding-unsteady-3-74.699997.dat.gz ││ vortex-shedding-unsteady-3-74.949997.dat.gz ││ vortex-shedding-unsteady-3-75.199997.dat.gz ││ vortex-shedding-unsteady-3-75.449997.dat.gz ││ vortex-shedding-unsteady-3-75.699997.dat.gz ││ vortex-shedding-unsteady-3-75.949997.dat.gz ││ vortex-shedding-unsteady-3-76.199997.dat.gz ││ vortex-shedding-unsteady-3-76.449997.dat.gz ││ vortex-shedding-unsteady-3-76.699997.dat.gz ││ vortex-shedding-unsteady-3-76.949997.dat.gz ││ vortex-shedding-unsteady-3-77.199997.dat.gz││ vortex-shedding-unsteady-3-77.699997.dat.gz ││ vortex-shedding-unsteady-3-77.949997.dat.gz ││ vortex-shedding-unsteady-3-78.199997.dat.gz ││ vortex-shedding-unsteady-3-78.449997.dat.gz ││ vortex-shedding-unsteady-3-78.699997.dat.gz ││ vortex-shedding-unsteady-3-78.949997.dat.gz ││ vortex-shedding-unsteady-3-79.199997.dat.gz ││ vortex-shedding-unsteady-3-79.449997.dat.gz ││ vortex-shedding-unsteady-3-79.699997.dat.gz ││ vortex-shedding-unsteady-3-79.949997.dat.gz ││ vortex-shedding-unsteady-3-80.199997.dat.gz ││ vortex-shedding-unsteady-3-80.449997.dat.gz ││ vortex-shedding-unsteady-3-80.699997.dat.gz ││ vortex-shedding-unsteady-3-80.950012.dat.gz ││ vortex-shedding-unsteady-3-81.200027.dat.gz ││ vortex-shedding-unsteady-3-81.450043.dat.gz ││ vortex-shedding-unsteady-3-81.700058.dat.gz ││ vortex-shedding-unsteady-3-81.950073.dat.gz ││ vortex-shedding-unsteady-3-82.200089.dat.gz ││ vortex-shedding-unsteady-3-82.450104.dat.gz ││ vortex-shedding-unsteady-3-82.700119.dat.gz ││ vortex-shedding-unsteady-3-82.950134.dat.gz ││ vortex-shedding-unsteady-3-83.200150.dat.gz ││ vortex-shedding-unsteady-3-83.450165.dat.gz ││ vortex-shedding-unsteady-3-83.700180.dat.gz ││ vortex-shedding-unsteady-3-83.950195.dat.gz ││ vortex-shedding-unsteady-3-84.200211.dat.gz ││ vortex-shedding-unsteady-3-84.450226.dat.gz ││ vortex-shedding-unsteady-3-84.700241.dat.gz ││ vortex-shedding-unsteady-3-84.950256.dat.gz ││ vortex-shedding-unsteady-3-85.200272.dat.gz ││ vortex-shedding-unsteady-3-85.450287.dat.gz ││ vortex-shedding-unsteady-3-85.700302.dat.gz ││ vortex-shedding-unsteady-3-85.950317.dat.gz ││ vortex-shedding-unsteady-3-86.200333.dat.gz ││ vortex-shedding-unsteady-3-86.450348.dat.gz ││ vortex-shedding-unsteady-3-86.700363.dat.gz ││ vortex-shedding-unsteady-3-86.950378.dat.gz ││ vortex-shedding-unsteady-3-87.200394.dat.gz ││ vortex-shedding-unsteady-3-87.450409.dat.gz ││ vortex-shedding-unsteady-3-87.700424.dat.gz ││ vortex-shedding-unsteady-3-87.950439.dat.gz ││ vortex-shedding-unsteady-3-88.200455.dat.gz││ vortex-shedding-unsteady-3-88.700485.dat.gz ││ vortex-shedding-unsteady-3-88.950500.dat.gz ││ vortex-shedding-unsteady-3-89.200516.dat.gz ││ vortex-shedding-unsteady-3-89.450531.dat.gz ││ vortex-shedding-unsteady-3-89.700546.dat.gz ││ vortex-shedding-unsteady-3-89.950562.dat.gz ││ vortex-shedding-unsteady-3-90.200577.dat.gz ││ vortex-shedding-unsteady-3-90.450592.dat.gz ││ vortex-shedding-unsteady-3-90.700607.dat.gz ││ vortex-shedding-unsteady-3-90.950623.dat.gz ││ vortex-shedding-unsteady-3-91.200638.dat.gz ││ vortex-shedding-unsteady-3-91.450653.dat.gz ││ vortex-shedding-unsteady-3-91.700668.dat.gz ││ vortex-shedding-unsteady-3-91.950684.dat.gz ││ vortex-shedding-unsteady-3-92.200699.dat.gz ││ vortex-shedding-unsteady-3-92.450714.dat.gz ││ vortex-shedding-unsteady-3-92.700729.dat.gz ││ vortex-shedding-unsteady-3.cas.gz│││└─Result-TUT_07││ cfd_post.cst││ point-4-y-velocity-final.out││ point-4-y-velocity.out││ sequence-1.mpeg││ vectors.mp4││ vortex-shedding-coarse-steady.cas.gz││ vortex-shedding-coarse-steady.dat.gz││ vortex-shedding-unsteady-final.cas.gz││ vortex-shedding-unsteady-final.dat.gz││ vortex-shedding-unsteady.cas.gz││ vortex-shedding-unsteady.dat.gz│││├─ADDITIONAL-FILES││ q-criterion2D.scm││ velocity.fft│││└─ANIMATION-FILES│ sequence-1.cxa│ sequence-1.mpeg│ sequence-1_0000.hmf│ sequence-1_0001.hmf│ sequence-1_0002.hmf│ sequence-1_0003.hmf│ sequence-1_0005.hmf │ sequence-1_0006.hmf │ sequence-1_0007.hmf │ sequence-1_0008.hmf │ sequence-1_0009.hmf │ sequence-1_0010.hmf │ sequence-1_0011.hmf │ sequence-1_0012.hmf │ sequence-1_0013.hmf │ sequence-1_0014.hmf │ sequence-1_0015.hmf │ sequence-1_0016.hmf │ sequence-1_0017.hmf │ sequence-1_0018.hmf │ sequence-1_0019.hmf │ sequence-1_0020.hmf │ sequence-1_0021.hmf │ sequence-1_0022.hmf │ sequence-1_0023.hmf │ sequence-1_0024.hmf │ sequence-1_0025.hmf │ sequence-1_0026.hmf │ sequence-1_0027.hmf │ sequence-1_0028.hmf │ sequence-1_0029.hmf │ sequence-1_0030.hmf │ sequence-1_0031.hmf │ sequence-1_0032.hmf │ sequence-1_0033.hmf │ sequence-1_0034.hmf │ sequence-1_0035.hmf │ sequence-1_0036.hmf │ sequence-1_0037.hmf │ sequence-1_0038.hmf │ sequence-1_0039.hmf │ sequence-1_0040.hmf │ sequence-1_0041.hmf │ sequence-1_0042.hmf │ sequence-1_0043.hmf │ sequence-1_0044.hmf │ sequence-1_0045.hmf │ sequence-1_0046.hmf │ sequence-1_0047.hmf│ sequence-1_0049.hmf │ sequence-1_0050.hmf │ sequence-1_0051.hmf │ sequence-1_0052.hmf │ sequence-1_0053.hmf │ sequence-1_0054.hmf │ sequence-1_0055.hmf │ sequence-1_0056.hmf │ sequence-1_0057.hmf │ sequence-1_0058.hmf │ sequence-1_0059.hmf │ sequence-1_0060.hmf │ sequence-1_0061.hmf │ sequence-1_0062.hmf │ sequence-1_0063.hmf │ sequence-1_0064.hmf │ sequence-1_0065.hmf │ sequence-1_0066.hmf │ sequence-1_0067.hmf │ sequence-1_0068.hmf │ sequence-1_0069.hmf │ sequence-1_0070.hmf │ sequence-1_0071.hmf │ sequence-1_0072.hmf │ sequence-1_0073.hmf │ sequence-1_0074.hmf │ sequence-1_0075.hmf │ sequence-1_0076.hmf │ sequence-1_0077.hmf │ sequence-1_0078.hmf │ sequence-1_0079.hmf │ sequence-1_0080.hmf │ sequence-1_0081.hmf │ sequence-1_0082.hmf │ sequence-1_0083.hmf │ sequence-1_0084.hmf │ sequence-1_0085.hmf │ sequence-1_0086.hmf │ sequence-1_0087.hmf │ sequence-1_0088.hmf │ sequence-1_0089.hmf │ sequence-1_0090.hmf │ sequence-1_0091.hmf│ sequence-1_0093.hmf│ sequence-1_0094.hmf│ sequence-1_0095.hmf│ sequence-1_0096.hmf│ sequence-1_0097.hmf│ sequence-1_0098.hmf│ sequence-1_0099.hmf│ sequence-1_0100.hmf│ sequence-1_0101.hmf│ sequence-1_0102.hmf│ sequence-1_0103.hmf│ sequence-1_0104.hmf│ sequence-1_0105.hmf│ sequence-1_0106.hmf│ sequence-1_0107.hmf│ sequence-1_0108.hmf│ sequence-1_0109.hmf│ sequence-1_0110.hmf│ sequence-1_0111.hmf│ sequence-1_0112.hmf│ sequence-1_0113.hmf│ sequence-1_0114.hmf│ sequence-1_0115.hmf│ sequence-1_0116.hmf│ sequence-1_0117.hmf│ sequence-1_0118.hmf│ sequence-1_0119.hmf│├─fluent-heat-transfer││ ht-01-intro-tut-04-periodic-flow-heat.pdf││ ht-02-intro-tut-07-radiation-and-convection.pdf ││ ht-03-intro-tut-08-DO-radiation.pdf││ ht-04-intro-tut-24-solidification.pdf││ ht-05-conjugate-heat-transfer.pdf││ ht-06-compact-heat-exchanger.pdf││ ht-07-macro-heat-exchanger.pdf││ ht-08-head-lamp.pdf│││├─ht-01-intro-tut-04-periodic-flow-heat│││ tubebank.msh│││││└─solution_files││tubebank.cas.gz││tubebank.dat.gz│││├─ht-02-intro-tut-07-radiation-and-convection │││ rad.msh.gz│││││└─solution_files││rad_1.s2s.gz││rad_10.cas.gz││rad_10.dat.gz││rad_10.s2s.gz││rad_100.cas.gz││rad_100.dat.gz││rad_100.s2s.gz││rad_1600.cas.gz││rad_1600.dat.gz││rad_1600.s2s.gz││rad_400.cas.gz││rad_400.dat.gz││rad_400.s2s.gz││rad_800.cas.gz││rad_800.dat.gz││rad_800.s2s.gz││rad_a_1.cas.gz││rad_b_1.cas.gz││rad_b_1.dat.gz││rad_partial.cas.gz││rad_partial.dat.gz││rad_partial.s2s.gz││tp_1.xy││tp_10.xy││tp_100.xy││tp_1600.xy││tp_400.xy││tp_800.xy││tp_partial.xy│││├─ht-03-intro-tut-08-DO-radiation│││ do.msh.gz│││││└─solution_files││do.cas.gz││do.dat.gz││do_2x2_10x10_pix.cas.gz││do_2x2_10x10_pix.dat.gz││do_2x2_1x1.xy││do_2x2_2x2_pix.cas.gz││do_2x2_2x2_pix.dat.gz││do_2x2_2x2_pix.xy││do_2x2_3x3_div.cas.gz││do_2x2_3x3_div.dat.gz││do_2x2_3x3_div.xy││do_2x2_3x3_pix.cas.gz││do_2x2_3x3_pix.dat.gz││do_2x2_3x3_pix.xy││do_3x3_3x3_div.cas.gz││do_3x3_3x3_div.dat.gz││do_3x3_3x3_div.xy││do_3x3_3x3_div_baf_int.xy ││do_3x3_3x3_div_df1.cas.gz ││do_3x3_3x3_div_df1.dat.gz ││do_3x3_3x3_div_df=1.xy ││do_3x3_3x3_div_int.cas.gz ││do_3x3_3x3_div_int.dat.gz ││do_5x5_3x3_div.cas.gz││do_5x5_3x3_div.dat.gz││do_5x5_3x3_div.xy│││├─ht-04-intro-tut-24-solidification│││ solid.msh│││││└─solution_files││solid.cas.gz││solid.dat.gz││solid0.cas.gz││solid0.dat.gz││solid01.cas.gz││solid01.dat.gz││solid5.cas.gz││solid5.dat.gz│││├─ht-05-conjugate-heat-transfer│││ chip3d.msh.gz│││││└─solution_files││chip3d-adapt1.cas.gz││chip3d-adapt1.dat.gz││chip3d-adapt2.cas.gz││chip3d.cas.gz││chip3d.dat.gz││surf-mon-1.out││temp-0.xy││temp-1.xy││temp-2.xy││velocity-0.xy││velocity-1.xy││velocity-2.xy││xwss-0.xy││xwss-1.xy││xwss-2.xy│││├─ht-06-compact-heat-exchanger │││ htx.msh.gz│││││└─solution_files││htx-energy.cas.gz││htx-energy.dat.gz││htx-eqn.cas.gz││htx-eqn.dat.gz││htx-final.cas.gz││htx-final.dat.gz││htx-setup.cas.gz││htx-setup.dat.gz││surf-mon-1.out│││├─ht-07-macro-heat-exchanger │││ rad.tab│││ wedge.msh.gz│││││└─solution_files││wedge1.cas.gz││wedge1.dat.gz││wedge2.cas.gz││wedge2.dat.gz││wedge3.cas.gz││wedge3.dat.gz││wedge4.cas.gz││wedge4.dat.gz│││└─ht-08-head-lamp││ head-lamp.msh.gz│││└─solution_fi les│ auto-hlamp.cas.gz│ auto-hlamp.dat.gz│ head-lamp-t.out│ hed-lamp-v.out│├─multiphase-fluent││ 01-hfilm.pdf││ 02-boil.pdf││ 03-nucleate_boil.pdf││ 04-dambreak.pdf││ 05-sloshing.pdf││ 06-bubble-col.pdf││ 07-bubble-break.pdf││ 08-inkjet.pdf││ 09-sparger.pdf││ 10-pbed-reactor.pdf││ 11-ddpm.pdf││ 12-dm-ship-wave.pdf││ 13-udf-clarifier.pdf││ 14-udf-fbed.pdf│││├─tut-01-hfilm│││ boiling.c│││ test-2d.msh.gz│││││└─solution_files│││ hfilm_input_files.tar.zg │││ nusselt-1.out│││ test-2d-1-00100.dat│││ test-2d-1-00200.dat│││ test-2d-1-00300.dat│││ test-2d-1-00400.dat│││ test-2d-1-00500.dat│││ test-2d-1-00600.dat│││ test-2d-1-00700.dat│││ test-2d-1-00800.dat│││ test-2d-1-00900.dat│││ test-2d-1-01000.dat│││ test-2d-1-01100.dat│││ test-2d-1-01200.dat│││ test-2d-1-01300.dat│││ test-2d-1-01400.dat│││ test-2d-1-01500.dat│││ test-2d-1-01600.dat│││ test-2d-1-01700.dat│││ test-2d-1-01800.dat│││ test-2d-1-01900.dat│││ test-2d-1-02000.dat│││ test-2d-1-02100.dat│││ test-2d-1-02200.dat│││ test-2d-1-02300.dat│││ test-2d-1-02400.dat│││ test-2d-1-02500.dat│││ test-2d-1-02600.dat│││ test-2d-1-02700.dat│││ test-2d-1-02800.dat│││ test-2d-1-02900.dat│││ test-2d-1-03000.dat│││ test-2d-1-03100.dat│││ test-2d-1-03200.dat│││ test-2d-1-03300.dat│││ test-2d-1-03400.dat│││ test-2d-1-03500.dat│││ test-2d-1-03600.dat│││ test-2d-1-03700.dat│││ test-2d-1-03800.dat│││ test-2d-1-03900.dat│││ test-2d-1-04000.dat│││ test-2d-1.cas│││ vol-mon-1.out│││││└─libudf││├─ntx86│││└─2ddp│││boiling.obj│││libudf.dll│││libudf.exp│││libudf.lib│││log│││makefile│││udf_names.c │││udf_names.obj │││user_nt.udf│││││├─src│││ boiling.c│││││└─win64││└─2ddp││boiling.obj││libudf.dll││libudf.exp││libudf.lib││log││makefile││ud_io1.h││udf_names.c ││udf_names.obj ││user_nt.udf│││├─tut-02-boil│││ boil.msh.gz│││││└─solution_files││boil-3-00300.dat.gz││boil-3-01000.dat.gz││boil-3.cas.gz│││├─tut-03-nucleate-boil│││ boiling-conjugate.msh│││││└─solution_files││boil-final.cas.gz││boil-final.dat.gz││boil-init.cas.gz││boil-init.dat.gz││boil-single-phase.cas.gz ││boil-single-phase.dat.gz ││liquid-outlet.prof││surf-mon-1.out││surf-mon-2.out│││├─tut-04-dambreak│││ dambreak.msh.gz│││││└─solution_files││dambreak-100.cas.gz││dambreak-100.dat.gz││dambreak-50.cas.gz││dambreak-50.dat.gz││dambreak-80.cas.gz││dambreak-80.dat.gz││dambreak.cas.gz││dambreak.dat.gz│││├─tut-05-sloshing│││ ft11.msh.gz│││││└─solution_files││├─baffles│││ baffles-data-file-4-02060.dat.gz │││ baffles-data-file-4-02080.dat.gz │││ baffles-images.zip│││ baffles.jou│││ ft11.msh.gz│││ operating.cas.gz│││ t=0.0s.cas.gz│││ t=0.0s.dat.gz│││ t=0.45s.cas.gz│││ t=0.45s.dat.gz│││ t=1.25s.cas.gz│││ t=1.25s.dat.gz│││ t=1.50s.cas.gz│││ t=1.50s.dat.gz│││ t=1.5s.cas.gz│││ t=1.5s.dat.gz│││ t=2.5s.cas.gz│││ t=2.5s.dat.gz│││││└─no-baffles││ no-baffles-data-file-4-02760.dat.gz ││ no-baffles-data-file-4-02780.dat.gz ││ no-baffles-images.zip││ no-baffles.jou││ t=0.0s.cas.gz││ t=0.0s.dat.gz││ t=0.45s.cas.gz││ t=0.45s.dat.gz││ t=0s.cas.gz││ t=0s.dat.gz││ t=1.25s.cas.gz││ t=1.25s.dat.gz││ t=1.5s.cas.gz││ t=1.5s.dat.gz││ t=2.5s.cas.gz││ t=2.5s.dat.gz││ tiff-no-baffles.zip │││├─tut-06-bubble-col│││ becker.msh│││││└─solution_files││becker-1-00200.dat.gz ││becker-1-00400.dat.gz ││becker-1-00600.dat.gz ││becker-1-00800.dat.gz ││becker-1-01000.dat.gz ││becker-1-01200.dat.gz ││becker-1-01400.dat.gz ││becker-1-01600.dat.gz ││becker-1-01800.dat.gz ││becker-1-02000.dat.gz ││becker-1-02200.dat.gz ││becker-1-02400.dat.gz ││becker-1-02600.dat.gz ││becker-1-02800.dat.gz ││becker-1-03000.dat.gz ││becker-1-03200.dat.gz ││becker-1-03400.dat.gz ││becker-1-03600.dat.gz ││becker-1-03800.dat.gz ││becker-1-04000.dat.gz ││becker-1-04200.dat.gz ││becker-1-04400.dat.gz ││becker-1-04600.dat.gz ││becker-1-04800.dat.gz ││becker-1-05000.dat.gz ││becker-1.cas.gz││becker.cas.gz││becker.dat.gz││vel-vectors.cxa││vel-vectors_0000.hmf ││vel-vectors_0001.hmf ││vel-vectors_0002.hmf ││vel-vectors_0003.hmf ││vel-vectors_0004.hmf ││vel-vectors_0005.hmf ││vel-vectors_0006.hmf││vel-vectors_0007.hmf ││vel-vectors_0008.hmf ││vel-vectors_0009.hmf ││vel-vectors_0010.hmf ││vel-vectors_0011.hmf ││vel-vectors_0012.hmf ││vel-vectors_0013.hmf ││vel-vectors_0014.hmf ││vel-vectors_0015.hmf ││vel-vectors_0016.hmf ││vel-vectors_0017.hmf ││vel-vectors_0018.hmf ││vel-vectors_0019.hmf ││vel-vectors_0020.hmf ││vel-vectors_0021.hmf ││vel-vectors_0022.hmf ││vel-vectors_0023.hmf ││vel-vectors_0024.hmf ││vof.cxa││vof_0000.hmf││vof_0001.hmf││vof_0002.hmf││vof_0003.hmf││vof_0004.hmf││vof_0005.hmf││vof_0006.hmf││vof_0007.hmf││vof_0008.hmf││vof_0009.hmf││vof_0010.hmf││vof_0011.hmf││vof_0012.hmf││vof_0013.hmf││vof_0014.hmf││vof_0015.hmf││vof_0016.hmf││vof_0017.hmf││vof_0018.hmf││vof_0019.hmf││vof_0020.hmf││vof_0021.hmf││vof_0022.hmf││vof_0023.hmf││vof_0024.hmf│││├─tut-07-bubble-break│││ bubcol_new2.msh.gz│││││└─solution_files││bubcol-final.cas.gz││bubcol-final.dat.gz││bubcol_new2-initial.cas.gz ││bubcol_new2-initial.dat.gz ││surf-mon-1.out││surf-mon-2.out││surf-mon-3.out│││├─tut-08-inkjet│││ inkjet.msh.gz│││ inlet1.c│││ udfconfig.h│││││└─solution_files││inkjet-1-00100.dat.gz││inkjet-1-00200.dat.gz││inkjet-1-00300.dat.gz││inkjet-1-00400.dat.gz││inkjet-1-00500.dat.gz││inkjet-1-00600.dat.gz││inkjet-1-00700.dat.gz││inkjet-1-00800.dat.gz││inkjet-1-00900.dat.gz││inkjet-1-01000.dat.gz││inkjet-1-01100.dat.gz││inkjet-1-01200.dat.gz││inkjet-1-01300.dat.gz││inkjet-1-01400.dat.gz││inkjet-1-01500.dat.gz││inkjet-1.cas.gz││inkjet-final.cas.gz││inkjet-final.dat.gz││inkjet.cas.gz││inkjet.dat.gz│││├─tut-09-sparger│││ sparger.msh.gz│││││└─solution_files。

FLUENT_UDF官方培训教程

FLUENT_UDF官方培训教程

FLUENT_UDF官方培训教程
必须原创
FLUENT UDF全称为Fluent User Defined Functions,是ANSYS Fluent有限元分析软件的一种高级应用技术,主要用于定制流体、多相流及热传导模拟中的特殊调整元件。

本文介绍如何使用FLUENT-UDF进行实际模拟的培训教程。

一、FLUENTUDF的概念
FLUENT UDF是一种定制的技术,它可以灵活地增强Fluent本身的模拟能力,并让用户能够自定义函数来调整流体、多相流及热传导模拟中的特殊参数。

FLUENT UDF是一种可以定义特殊参数和条件的技术,它可以让Fluent本身的模拟更加强大。

用户可以根据实际的需求自定义这些特殊参数,从而实现更加全面和精确的模拟。

二、FLUENTUDF的步骤
2.编写UDF函数:
UDF函数可以用C或Fortran语言编写,也可以用Fluent自带的UDFEasy编译器编写。

编写UDF函数的基本步骤是:
(1)编写UDF函数的声明,它在编译器的第一行声明,用于定义函数的相关参数;
(2)编写函数代码,用于计算流体及热传导的相关参数;
(3)编写函数的结束部分,使函数返回正确的值并运行成功。

ANSYS官方帮助文件05-udf

ANSYS官方帮助文件05-udf

ANSYS官⽅帮助⽂件05-udfTutorial:Modeling Uniform Fluidization in2D Fluidized BedIntroductionThe prediction of pressure drop in an uniformly?uidized bed is a problem of long standing interest in the process industry.The Eulerian models in ANSYS FLUENT provide an impor-tant modeling tool for studying dense phase particulate?ow involving complex inter-phase momentum transfer.Despite rigorous mathematical modeling of the associated physics,the drag laws used in the model continue to be semi-empirical in nature.Therefore,it is crucial to use a drag law that correctly predicts the incipient or minimum?uidization conditions where the bed of particles is essentially in a state of suspension as a result of the balance between interfacial drag and body forces.The purpose of this tutorial is to study the hydrodynamics and bubble formation in a ?uidized bed over a period of time.It also demonstrates how to customize a drag law for granular gas-solid?ow.This tutorial demonstrates how to do the following:Customize a drag law for granular gas-solidow.Use the Eulerian models to predict the pressure drop in an uniformlyuidized bed.Solve the case using appropriate solver settings.Postprocess the resulting data.PrerequisitesThis tutorial is written with the assumption that you have completed Tutorial1from the ANSYS FLUENT12.0Tutorial Guide,and that you are familiar with the ANSYS FLUENT navigation pane and menu structure.Some steps in the setup and solution procedure will not be shown explicitly.This tutorial will not cover the mechanics of using the Eulerian models.It will focus on the application of these models.For more information refer to Section24.5Setting Up the Eulerian Model in the ANSYS FLUENT User’s Guide.For information about user-de?ned fucntions(UDF)refer to the ANSYS FLUENT UDF Manual.Modeling Uniform Fluidization in2D Fluidized BedProblem DescriptionThe default drag law in ANSYS FLUENT is the Syamlal-O’Brien drag law.This law works for a large variety of problems,but has to be tuned properly for predicting the minimum ?uidization conditions accurately.The default Syamlal-O’brien is as follows:The?uid-solid exchange coe?cient isK sl=3αsαlρl4v2r,s d sC DRe sv r,s| v s? v l|where v2r,s is the terminal velocity coe?cient for the solid phase.v r,s=0.5 A?0.06Re s+ (0.06Re s)2+0.12Re s(2B?A)+A2with A=α4.14l and B=0.8α1.28lforαl≤0.85and with B=α2.65lforαl>0.85The default constants of0.8and2.65predict a minimum?uidization of21cm/s.The experimentally observed minimum? uidization for this particular case is8cm/s.Therefore, by changing the constants we can tune the drag law to predict minimum? uidization at 8cm/s.After some mathematical manipulation,these constants come out to be0.281632and9.07696respectively.Therefore,these values have to be used to predict the correct bed behavior and are passed to the code through user-de?ned functions.The problem considered is a1m x0.15m?uidized bed as shown in Figure1.The inlet air enters in at0.25m/s and the top is modeled as a pressure outlet.The bed is packed with granular solids at0.55volume fraction(close topacking).Figure1:Problem Speci?cationModeling Uniform Fluidization in2D Fluidized Bed Preparation1.Copy the?les,bp.msh.gz and bp drag.c to the working folder./doc/7ae06ac9a1c7aa00b52acba0.html e FLUENT Launcher to start the2D version of ANSYS FLUENT.For more information about FLUENT Launcher see Section1.1.2Starting ANSYS FLU-ENT Using FLUENT Launcher in the ANSYS FLUENT12.0User’s Guide.3.Enable Double-Precision in the Options list.4.Click the UDF Compiler tab and make sure that Setup Compilation Environment forUDF is enabled.The path to the.bat?le which is required to compile the UDF will be displayed as soon as you enable Setup Compilation Environment for UDF.If the UDF Compiler tab does not appear in the FLUENT Launcher dialog box by default, click the Show Additional Options>>button to view the additional settings.Note:The Display Options are enabled by default.Therefore,after you read in the mesh,it will be displayed in the embedded graphics window.Setup and SolutionNote:All entries in setting up this case are in SI units,unless otherwise speci?ed.Step1:Mesh1.Read the mesh?le bp.msh.gz.File?→Read?→Mesh...Figure2:Graphics Display of the MeshModeling Uniform Fluidization in2D Fluidized BedStep2:General1.Check the mesh.General?→CheckANSYS FLUENT will perform various checks on the mesh and will report the progress in the console.Ensure that the minimum volume reported is a positive number.2.Enable the transient solver by selecting Transient from the Time list.General?→TransientStep3:Models1.Select the Eulerian multiphase model.Models?→Multiphase?→Edit...(a)Select Eulerian from the Model selection list.(b)Retain the default settings and close the Multiphase Model dialog box.Step4:Materials1.Modify the properties for air.Materials?→air?→Create/Edit...(a)Enter1.2kg/m3for Density.(b)Enter1.8e-05kg/m-s for Viscosity.(c)Click Change/Create.2.De?ne a material called solids.Modeling Uniform Fluidization in2D Fluidized Bed(a)Enter solids for Name.(b)Enter2600kg/m3for Density and1.7894e-05kg/m-s for Viscosity.(c)Click Change/Create.A Question dialog box will appear asking if you want to overwrite air.Click No.3.Close the Create/Edit Materials dialog box.Step5:Compile the UDFThe UDF contains two arguments s col and f col.These refer to the indices of the phases appearing in the second and?rst columns of the table in the interaction dialog box respec-tively.Therefore in this case s col refers to the index of gas phase which is0and f col refers to the index for solids which is equal to1.De?ne?→User-De?ned?→Functions?→Compiled...1.Click the Add...button in the Source Files section to open the Select File dialog.2.Select the?le bp drag.c.3.Enter lib drag for Library Name.4.Click Build.A Warning dialog box will appear,warning you to make sure that the UDF source?lesare in the same folder that contains the case and data?les.Click OK to close the Warning dialog box.You can view the compilation history in the log?le that is saved in your working folder.5.Click Load to load the library.Modeling Uniform Fluidization in2D Fluidized BedStep6:Phases1.De?ne primary phase.Phases?→phase-1?→Edit...(a)Enter gas for Name.(b)Ensure air is selected from the Phase Material drop-down list.(c)Click OK to close the Primary Phase dialog box.2.De?ne secondary phase.Phases?→phase-2?→Edit...Modeling Uniform Fluidization in2D Fluidized Bed(a)Enter solid for Name.(b)Select solids from the Phase Material drop-down list.(c)Enable Granular.(d)Enter0.0003m for Diameter,and select syamlal-obrien from the Granular Viscositydrop-down list.(e)Retain the default values for the other parameters.(f)Click OK to close the Secondary Phase dialog box.Check the column numbers where the two phases appear in the Phase Interaction dialog box.In this case solid and gas appear in the?rst and second columns respectively.These columns are used to specify the phase indices in the argument list for the UDF.3.Set the drag coe?cient.(a)Select gas from the Phases selection list and click the Interaction...button toopen the Phase Interaction dialog box.i.Select user-de?ned from the drop-down list in the Drag Coe?cient group box.Modeling Uniform Fluidization in2D Fluidized BedA.Ensure that custom drag syam::lib drag is selected.B.Click OK to close the User-De?ned Functions dialog boxii.Click OK to close the Phase Interaction dialog box.(b)Similarly select the user de?ned function for solid(custom drag syam::lib drag).Step7:Boundary Conditions1.Set the boundary conditions for vinlet zone.Boundary Conditions?→vinlet(a)Select gas from the Phase drop-down list and click Edit....i.Select Components from the Velocity Speci?cation Method drop-down list.ii.Enter0.25m/s for Y-Velocity.iii.Click OK to close the Velocity Inlet dialog box.(b)Select solid from the Phase drop-down list and click the Edit...button to openthe Velocity Inlet dialog box.i.Click the Multiphase tab.ii.Ensure that Volume Fraction is0.iii.Click OK to close the Velocity Inlet dialog box.Modeling Uniform Fluidization in2D Fluidized Bed Step8:Operating ConditionsBoundary Conditions?→Operating Conditions...1.Enable Gravity and enter-9.81m/s2for Gravitational Acceleration in the Y direction.2.Enable Speci?ed Operating Density,and enter1.2kg/m3for Operating Density.3.Click OK to close the Operating Conditions dialog box.Step9:Solution1.Mark a region for adaption.Adapt?→Region...Modeling Uniform Fluidization in2D Fluidized Bed(a)Enter0.15m for X Max and Y Max respectively in the Input Coordinates groupbox.(b)Click Mark to mark the cells for re?nement.Note:Click Adapt to perform the re?nement immediately.(c)Close the Region Adaption dialog box.2.Set the solution control parameters.Solution Controls(a)Enter0.5for Pressure in the Under-Relaxation Factors group box.(b)Enter0.2for Momentum.(c)Enter0.4for Volume Fraction.3.Initialize the?ow with default values.Solution Initialization?→InitializeModeling Uniform Fluidization in2D Fluidized Bed 4.Patch the solids volume fraction for hexahedron-r0.Solution Initialization?→Patch...(a)Select solid from the Phase drop-down list.(b)Select Volume Fraction from the Variable selection list.(c)Enter0.55for Value.(d)Select hexahedron-r0from the Registers to Patch selection list.If you wish to patch a constant value,enter that value in the Value?eld.If you want to patch a previously-de?ned?eld function,enablethe Use Field Function option and select the appropriate function inthe Field Function list.(e)Click Patch and close the Patch dialog box.5.Enable autosaving of the data?les for every100time steps.Calculation Activities(a)Enter100for Autosave Every(Time Steps).6.Set up commands for animation.Calculation Activities(Execute Commands)?→Create/Edit...Modeling Uniform Fluidization in2D Fluidized Bed(a)Set2for De?ned Commands.(b)Enable Active for both commands.(c)Set10for Every for both commands.(d)Select Time Step from the When drop-down list for both.(e)Enter/display/contour/solid/vof for command-1.(f)Enter/display/hardcopy"vof-solids-%t.tiff"for command-2.(g)Click OK to close the Execute Commands dialog box.7.Set the graphics hardcopy format.File?→Save Picture...(a)Select TIFF from the Format list.(b)Select Color from the Coloring list.(c)Click Apply and close the Save Picture dialog box.8.Set up the contours display.Graphics and Animations?→Contours?→Set Up...(a)Enable Filled from the Options group box.(b)Select solid from the Phase drop-down list.(c)Select Phases...and Volume Fraction from the Contours of drop-down lists.(d)Click Display and close the Contours dialog box.9.Save the case?le(bp.cas.gz).File?→Write?→Case...10.Start the calculation.Run Calculation.(a)Enter0.001sec for Time Step Size.(b)Enter1400for Number of Time Steps.(c)Enable Extrapolate Variables.(d)Click Calculate.11.Save the data?le(bp.dat.gz).File?→Write?→Data...Modeling Uniform Fluidization in2D Fluidized BedStep10:Postprocessing1.Display contours of volume fraction.(a)Read the data?le for the200th time step(bp-1-00200.dat).File?→Read?→Data...(b)Display?lled contours of volume fraction for solid,at0.2sec(Figure3).Graphics and Animations?→Contours?→Set Up...Figure3:Contours of Volume Fraction of solid(t=0.2s)(c)Similarly display contours at0.9sec(Figure4),and1.4sec(Figure5).Figure4:Contours of Volume Fraction of solid(t=0.9s)Modeling Uniform Fluidization in2D Fluidized BedFigure5:Contours of Volume Fraction of solid(t=1.4s)2.View the animation for the?uidization process using the.tiff?les.ResultsTypically,the constants set to0.8and2.65in the default drag law have to be modi?ed to balance the interfacial drag with the weight of the bed at minimum?uidization.If this is not done,the correct bubbling pattern will not be predicted,leading toincorrect predictions of pressure drop which is the most important objective of such simulations.。

ANSYSFLUENT130UDF手册

ANSYSFLUENT130UDF手册

实例二:自定义辐射模型
问题描述
在某些涉及辐射传热的流动问题中,标准的辐射模型可能 无法满足需求,需要自定义辐射模型。
UDF实现方法
通过编写UDF,可以定义新的辐射模型,包括辐射传热方 程、辐射源项等,并将其嵌入到FLUENT中进行计算。
案例分析
以一个包含辐射传热的燃烧室流动为例,通过自定义辐射 模型,可以更准确地模拟燃烧室内的温度分布、热流密度 等。
欧拉-拉格朗日方法
跟踪离散相(如颗粒、液滴)在连续相中 的运动轨迹。
多相流界面追踪
捕捉和追踪不同相之间的界面,如自由表 面流动、分层流动等。
化学反应模型
详细化学反应机理
支持复杂化学反应的详细机理描述,包括基 元反应、反应速率常数等。
反应动力学模型
描述化学反应过程中的动力学行为,如反应 速率、活化能等。
ANSYSFLUENT130UDF手册
CONTENTS
• UDF基本概念与介绍 • UDF编程基础 • UDF在FLUENT中应用 • UDF高级功能实现 • UDF调试与优化技巧 • UDF实例分析与讨论
01
UDF基本概念与介绍
UDF定义及作用
定义
UDF(User-Defined Function)是 用户自定义函数,允许用户在ANSYS FLUENT中编写自己的代码来解决特 定问题。
实例三:复杂流动问题模拟
问题描述
对于某些复杂的流动问题,如多相流、化学反应流等,标 准的FLUENT模型可能无法直接处理,需要借助UDF进行 模拟。
UDF实现方法
通过编写UDF,可以实现复杂的流动问题模拟,包括多相 流模型、化学反应模型等,并将其嵌入到FLUENT中进行 计算。
案例分析

ansysfluent官方培训教程07udf

ansysfluent官方培训教程07udf

ansysfluent官方培训教程07udf一、教学内容本节课我们将学习Ansys Fluent官方培训教程的第七部分,主要内容包括UDF(UserDefined Functions)的入门和使用。

通过本节课的学习,学生将掌握如何使用UDF自定义边界条件、修改流场变量以及实现更复杂的功能。

二、教学目标1. 了解UDF的概念和作用;2. 学会使用UDF自定义边界条件;3. 掌握通过UDF修改流场变量的方法;4. 能够运用UDF实现简单的人工天气变化。

三、教学难点与重点重点:UDF的概念和作用、UDF的基本语法和使用方法。

难点:通过UDF修改流场变量、实现复杂功能。

四、教具与学具准备1. 电脑;2. Ansys Fluent软件;3. UDF示例文件;4. 教学PPT。

五、教学过程1. 实践情景引入:讲解通过UDF实现边界条件修改的实例,让学生了解UDF的作用和基本使用方法。

2. 知识讲解:详细讲解UDF的概念、基本语法和使用方法,让学生理解如何通过UDF实现自定义功能。

3. 例题讲解:分析并讲解UDF示例文件,让学生学会如何编写和应用UDF。

4. 随堂练习:让学生自行尝试修改示例UDF文件,观察修改后的流场变化,巩固所学知识。

5. 课堂讨论:引导学生探讨如何利用UDF实现更复杂的功能,如人工天气变化。

六、板书设计板书设计如下:1. UDF概念和作用2. UDF基本语法3. UDF使用方法4. UDF实现边界条件修改5. UDF实现流场变量修改6. UDF实现复杂功能示例七、作业设计1. 请用UDF实现一个自定义边界条件,并观察流场变化。

答案:自定义一个速度边界条件,使得入口速度为某一固定值。

2. 请用UDF修改流场中的某一变量,并观察变化。

答案:通过UDF修改流场中的密度值,使得某一区域密度增加。

3. 请尝试利用UDF实现一个简单的人工天气变化模型。

答案:通过UDF修改温度场,实现温度随时间的变化,模拟气温变化。

ANSYS的帮助文件使用说明

ANSYS的帮助文件使用说明

ANSYS的帮助⽂件使⽤说明ANSYS的帮助⽂件使⽤说明很多⽹友都曾觉得ANSYS使⽤起来有⼀定的难度,经常会遇到这样或那样的问题,但市⾯上的参考书⼜不尽如⼈意,那究竟有没有⽐较好的参数书?有的,个⼈认为ANSYS的帮助⽂件就是⼀本不错的参数书。

接下来就ANSYS在线帮助的使⽤做⼀些基本的介绍,希望能对初学者有所帮助。

ANSYS的帮助⽂件包括所有ANSYS命令解释及所有的GUI解释,还包括ANSYS各模块的分析指南,实例练习等。

⼀.进⼊帮助系统可以通过下列三种⽅式进⼊:1.进⼊ANSYS的操作界⾯后,在应⽤菜单中选取Help进⼊;2.在ANSYS程序组中选取Help System进⼊:Start Menu > Programs > ANSYS XX>Help Sy stem;3.在任何对话框中选取Help。

⼆.帮助系统的内容安排:点击帮助系统的⽬录,就看到如下的ANSYS帮助系统的整体内容安排:1.前⾯4个部分是与软件版本,安装,注册相关的信息,只需作相应的了解即可,如下:※Release Notes※ANSYS Installation and Configuration Guide for UNIX※ANSYS Installation and Configuration Guide for Windows※ANSYS, Inc. Licensing Guide2.接下来两个部分是⽐较重要的部分,ANSYS的命令和单元⼿册,对⽤到的命令和单元应作详细的了解和掌握。

※ANSYS Commands Reference※ANSYS Element Reference3.下⾯四个部分是ANSYS相关的操作⼿册,说明如下:※Operations Guide 基本界⾯,操作指南※Basic Analysis Procedures Guide 基础分析指南※Advanced Analysis Techniques Guide ⾼级分析指南※Modeling and Meshing Guide 建模与分⽹指南4.以下⼏个部分则是ANSYS分模块的分析指南,如下:※Structural Analysis Guide 结构分析指南※Thermal Analysis Guide 热分析指南※CFD FLOTRAN Analysis Guide 流体分析指南※Electromagnetic Field Analysis Guide 电磁场分析指南※Coupled-Field Analysis Guide 耦合场分析指南5.为更好的使⽤ANSYS⽅便,快捷的解决更多的⼯程实际问题,建议仔细学习以下⼏个部分:※APDL Programmer's Guide:APDL操作⼿册※ANSYS Troubleshooting Guide:ANSYS错误信息指南※Mechanical Toolbar:机械⼯具栏※ANSYS/LS-DYNA User's Guide:ANSYS/LS-DYNA操作指南※ANSYS Connection Users Guide:接⼝技术指南6.欲快速掌握ANSYS的使⽤,莫过于通过实例和练习,⽽ANSYS的帮助系统中则提供⼤量的例题及练习供⽤户参考,所以以下两个部分是经常光顾的。

2024版ansysfluent官方培训教程07udf

2024版ansysfluent官方培训教程07udf

选择合适的编程工 具
可以使用任何支持C语言的编程 工具来编写UDF程序,如 Microsoft Visual Studio、 Code:Blocks等。根据实际需求 选择合适的编程工具进行安装和 配置。
03
编写简单的UDF程 序
在了解基本语法和编程规范后, 可以尝试编写一个简单的UDF程 序,如计算流场中某点的速度大 小。在编写过程中,需要注意代 码的规范性和可读性。
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3
UDF定义及作用
01
UDF(User-Defined Function) 是用户自定义函数,允许用户在 ANSYS Fluent中编写自己的代 码来解决特定问题。
02
UDF可以用于定义边界条件、物 性参数、源项、控制方程等,扩 展了ANSYS Fluent的功能和灵 活性。
03
switch-case等,用于实现条 件判断。
循环结构包括for循环、while 循环和do-while循环,用于实 现重复执行某段代码的功能。
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在使用控制语句和循环结构时, 需要注意语法格式和正确使用 大括号({})来定义代码块。
13
UDF常用函数库介绍
数学函数库包含了常见的数学运算函数,如sin、 cos、sqrt等。
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不收敛问题
调整求解器设置、改进网格质量或调整边界条件,以提高求解收敛性。
21
性能优化建议
优化算法
选择更高效的算法和数据结构,减少计算量 和内存占用。
并行计算
利用ANSYS Fluent的并行功能,加速UDF 的计算过程。
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减少I/O操作
减少不必要的文件读写操作,以提高程序运 行效率。

ANSYSFLUENT培训教材UDF

ANSYSFLUENT培训教材UDF
DEFINE_INIT(my_init_function, domain) {
cell_t c; Thread *ct; real xc[ND_ND]; thread_loop_c(ct,domain) {
begin_c_loop (c,ct) { C_CENTROID(xc,c,ct); if (sqrt(ND_SUM(pow(xc[0]-0.5,2.),
Fluid (cell thread or zone)
Domain
Cell Thread
face Thread
Cells
Faces
为了在thread (zone)中获得数据,我们需要提供正确的指针,并 使用循环宏获得thread中的每个成员(cell or face)
A Pera Global Company © PERA China
– 所有的UDFs 以 DEFINE_ 宏开始
– x_velocity 将在 GUI中 出现
– thread 和 nv DEFINE_PROFILE 宏的参 数, 分别用来识别域和变量
– begin_f_loop宏通过 thread指针,对所有的面f 循环
F_CENTROID宏赋单元位置向 量给 x[]
点击 Interpret FLUENT 窗口会出现语言 如果没有错误,点击 Close
A Pera Global Company © PERA China
解释 vs. 编译
用户函数可以在运行时读入并解释,也可以编译形成共享库文件并和 FLUENT链接
解释 vs. 编译 – 解释
• 解释器是占用内存的一个大型程序 • 通过逐行即时执行代码 • 优势 – 不需要第三方编译器 • 劣势 – 解释过程慢,且占用内存

fluent udf 编译教程

fluent udf 编译教程

在使用Fluent软件进行模拟计算时,经常会遇到需要自定义用户子程序(User Defined Function,简称UDF)的情况。

UDF是Fluent中用户自己编写的函数,用于描述流场中的边界条件、源项等物理过程。

为了正确地使用UDF并进行模拟计算,我们需要了解如何编写和编译UDF。

本教程将向大家介绍如何使用ANSYS Fluent进行UDF的编译,并提供一些常见问题的解决方法。

一、准备工作在进行UDF编译之前,我们需要进行一些准备工作。

1. 确保已安装ANSYS Fluent软件,并且能够正常运行;2. 确保已安装C/C++编译器,常见的编译器有Microsoft Visual Studio、GCC等;3. 编写好UDF的源代码文件,可以使用任何文本编辑器编写,但建议使用支持C/C++语法高亮的编辑器,以便于排查语法错误。

二、设置Fluent编译环境在进行UDF编译之前,我们需要设置Fluent的编译环境,以确保编译器可以正确地识别Fluent的API。

1. 打开命令行终端(Windows系统为cmd,Linux/Unix系统为Terminal);2. 运行以下命令设置Fluent的编译环境:对于Windows系统:```bashcd C:\Program Files\ANSYS Inc\v200\fluentfluent 3d -i```对于Linux/Unix系统:```bashcd /usr/ansys_inc/v200/fluent./fluent 3d -t xxx -g -i```其中,xxx是你的图形界面类型,可以根据你实际的图形界面类型进行替换,一般为Gl 或 X11。

运行上述命令后,Fluent将会启动,并且设置了编译环境。

在Fluent 的命令行界面中,我们可以进行UDF的编译和加载。

三、编译UDF在设置了Fluent的编译环境后,我们可以开始编译UDF了。

1. 将编写好的UDF源代码文件(后缀名通常为.c或.cpp)放置在Fluent的工作目录中;2. 在Fluent的命令行界面中,输入以下命令进行编译:```bash/define/user-definedpiled-functions load my_udf-name/define/user-definedpiled-functionspile my_udf-name/define/user-definedpiled-functions write my_udf-name/exit```其中,my_udf-name是你的UDF源代码文件的文件名(不包括后缀名),例如my_udf。

ANSYS中文帮助文件

ANSYS中文帮助文件

ANSYS文献工作指南手册在ANSYS 产品文献工作确定的形式下面已列出。

他们包括程序的说明,命令,要素和理论的细节需要使用ANSYS。

每手工跟随的简短描述。

命令参考: 描述全部ANSYS命令,按字母顺序。

这决定性参考适合正确使用,提供联系的菜单路径,产品应用性和使用纸币。

要素参考: 描述全部ANSYS 要素,按数字大小排列。

这是正确的元件类型输入“与”输出的主要参考,为每种要素的每个选项提供全面的说明。

包括一份每种ANSYS 要素的特性的照片的目录。

操作引导: 描述基本ANSYS 操作(例如起动),停止,相互作用或者分批操纵,使用帮助,以及使用的这图形用户界面(GUI) .基本的分析引导: 描述应用于任何类型分析的一般的任务,包括把负荷用于一个模型,获得一个解决办法,并且使用ANSYS 计划的绘图评论结果的能力。

高级分析技术引导: 讨论技术通常用于复分析或者凭经验ANSYS 用户,包括设计最优化,手工重新区划,周期的对称性,旋转的结构,submodeling,子结构化,构件模态综合和横断面。

建模和啮合引导: 解释怎样创建一个有限元模型和网捕它。

分配ANSYS引导: 解释怎样配置分配的处理环境并且继续一个分配的分析。

结构分析引导: 描述怎样进行下列结构分析:静止,情态,谐波,瞬时,范围,弯曲,非线性,物质的曲线配件,垫片共同模拟,裂缝,合成,疲劳,p 方法,梁和壳。

接触技术引导: 描述怎样执行接点分析(地面对地面,节点对表面,节点对节点) 并且描述其他有关接触的特征,例如多点的限制和点焊。

Multibody 分析引导: 描述怎样进行一次multibody 模拟分析一个使相互连接的包括灵活和/或硬的组成部分的身体的系统的动态反应。

热分析引导: 描述怎样做稳态或者瞬时的热分析。

流体分析引导: 描述怎样进行包括计算流体动力学,声学和薄膜的易流动的流量分析。

低频的电磁分析引导: 为做瞬时,静止,或者谐波磁力分析解释技术;稳态电流传导;quasistatic谐波和瞬时时间电;静电;与电路。

fluentudf环境变量的设置

fluentudf环境变量的设置

ANSYS fluent udf环境变量的设置初学udf,还没进入主题就被udf问题搞死了,摸索了一两天终于让我搞出了点名堂,本人用的是ANSYS 和vc .不多说,先把ANSYS 和vc都装上,网上有教程安装的,一步步来别跳步。

最好把vc6也装一下,因为里面有的东西设置环境变量要用到。

先不要打开软件。

设置环境变量:1.C:\Program Files\ANSYS Inc\v150\fluent\ntbin\win64目录下双击setenv和remenv2.设置环境变量:INCLUDEC:\Program Files (x86)\Microsoft Visual Studio \VC\include;C:\Program Files (x86)\Microsoft SDKs\Windows\\Include;LIBC:\Program Files (x86)\Microsoft Visual Studio \VC\lib\amd64;C:\Program Files (x86)\Microsoft SDKs\Windows\\Lib\x64;C:\Program Files (x86)\Microsoft Visual Studio \VC\atlmfc\lib;PATHC:\Program Files (x86)\Microsoft Visual Studio \VC\bin\amd64;C:\Program Files (x86)\Microsoft Visual Studio \Common7\IDE;找个udf文件,注意udf是支持三维还是二维的,打开fluent , 设置工作目录。

如下:接着就是编译了,不用打开case的,直接就可以define ….如果出现什么 xcopy….我们找到C:\Windows\System32里面的xcopy复制到C:\Program Files (x86)\Microsoft Visual Studio \VC\bin;C:\Program Files (x86)\Microsoft Visual Studio \VC\bin\amd64;如果出现“size_t”: 重定义;不同的基类型,可能是你的udf文件有问题。

UDF是什么?

UDF是什么?

UDF是什么?注:本文翻译自UDF手册,详细信息可查阅fluent UDF手册。

用户定义函数(UDF)是一个C函数,可以通过ANSYS FLUENT求解程序动态加载该函数以增强其标准功能。

例如,你可以使用UDF完成以下的事情:·自定义边界条件、材料物性参数、表面和体积反应速率、ANSYS FLUENT输运方程中的源项、用户定义标量(UDS)传输方程中的源项、扩散函数等。

·在每次迭代的基础上调整计算值。

·解的初始化。

·执行UDF的异步(按需)执行。

·在迭代结束时执行,在退出ANSYS FLUENT时执行,或在加载已编译的UDF库时执行。

·增强后处理。

·完善现有ANSYS FLUENT模型(如discrete phase model, multiphase mixturemodel, discrete ordinates radiation model)。

udf由一个扩展名为.c定义(例如,myudf.c)。

一个源文件可以包含单个UDF或多个UDF,你可以定义多个源文件。

有关C语言编程的一些基本信息,请参见附录A。

udf 是使用ANSYS FLUENT提供的DEFINE macros定义的。

它们使用外部的宏和函数(也由ANSYS FLUENT提供)进行编码,这些宏和函数访问ANSYS FLUENT求解器数据并执行其他任务。

每个UDF都必须在源代码文件的开头包含UDF .h文件包含指令(#include“UDF .h”),这样DEFINE宏和ANSYS FLUENT提供的其他宏和函数的定义以及它们的编译才能执行。

包含udf的源文件可以在ANSYS FLUENT中进行解释或编译·对于解释过的udf,源文件在运行时通过单步处理直接解释和加载。

·对于已编译的udf,该过程涉及两个单独的步骤。

首先建立一个共享的目标代码库,然后将其加载到ANSYS FLUENT中。

64位ANSYSFLUENT编译UDF方法

64位ANSYSFLUENT编译UDF方法

64位ANSYSFLUENT编译UDF⽅法ANSYS FLUENT 12.x 13.x版下使⽤Visual Studio 2010编译UDF的设置⽅法COMSOL出了点问题,只能重装系统搞定。

神马软件都要重装啊,今天装好ANSYS后,打开FLUENT界⾯时,灵感闪现,想出下⾯的⽅法设置UDF编译环境。

其实ANSYS版的FLUENT⽤UDF是不需要到系统环境变量⾥⾯设置path,include,lib的,如果您⽤的是Visual Studio 2010及后续版本,只需要按⼀定的规则设置udf.bat⽂件就⾏了。

从udf.bat⽂件结构看,VS版本在VS2010以前的都可以不⽤设置,即可使⽤。

实现⽅法,以Win7 X64位ANSYS X64位为例:1.找到fluent安装⽬录下的udf.bat(C:\Program Files\ANSYS Inc\v121\fluent\ntbin\win64\udf.bat)⽤⽂本编辑器修改udf.bat:添加echo trying to find MS C compiler, version 10.0....set MSVC_DEFAULT=%ProgramFiles(x86)%\Microsoft Visual Studio 10.0if exist "%MSVC_DEFAULT%\vC\vcvarsall.bat" set MSVC=%MSVC_DEFAULT%if not "%MSVC%" == "" goto msvc_env100set MSVC_DEFAULT=%ProgramFiles%\Microsoft Visual Studio 10.0if exist "%MSVC_DEFAULT%\vC\vcvarsall.bat" set MSVC=%MSVC_DEFAULT%if not "%MSVC%" == "" goto msvc_env100:msvc_env100set MSVC_VERSION=100call "%MSVC%\VC\vcvarsall.bat" amd64goto ms_c_end注:如果Visual Studio安装到其他盘,(可能)需要修改路径,⽐如装到D盘Program Files下,便这样添加:set MSVC_DEFAULT=d:\Program Files\Microsoft Visual Studio 10.0if exist "%MSVC_DEFAULT%\vC\vcvarsall.bat" set MSVC=%MSVC_DEFAULT%if not "%MSVC%" == "" goto msvc_env100:msvc_env100set MSVC_VERSION=100call "%MSVC%\VC\vcvarsall.bat" amd64goto ms_c_end2. 保存该⽂件即可实现编译环境设置3. 打开FLUENT,确认勾选UDF compiler下的setup compilation environment for UDF:附:环境变量设置⽅法:include中添加:64位系统:%ProgramFiles(x86)%\Microsoft Visual Studio 10.0\VC\include;%ProgramFiles(x86)%\MicrosoftSDKs\Windows\v7.0A\Include;32位系统:%ProgramFiles%\Microsoft Visual Studio 10.0\VC\include;%ProgramFiles%\Microsoft SDKs\Windows\v7.0A\Include; path 中添加:64位系统:%ProgramFiles(x86)%\Microsoft Visual Studio 10.0\VC\lib;%ProgramFiles(x86)%\Microsoft SDKs\Windows\v7.0A\lib32位系统:%ProgramFiles%\Microsoft Visual Studio 10.0\VC\lib;%ProgramFiles%\Microsoft SDKs\Windows\v7.0A\liblib中添加:64位系统:%ProgramFiles(x86)%\Microsoft Visual Studio 10.0\VC\bin;%ProgramFiles(x86)%\Microsoft Visual Studio10.0\VC\bin\amd64;%ProgramFiles(x86)%\Microsoft Visual Studio 10.0\Common7\IDE;%ProgramFiles(x86)%\Microsoft Visual Studio 10.0\Common7\Tools;32位系统:%ProgramFiles%\Microsoft Visual Studio 10.0\VC\bin;%ProgramFiles%\Microsoft Visual Studio10.0\VC\bin\amd64;%ProgramFiles%\Microsoft Visual Studio 10.0\Common7\IDE;%ProgramFiles%\Microsoft Visual Studio 10.0\Common7\Tools;天乐树。

15.NX5_udf的使用和创建UG

15.NX5_udf的使用和创建UG

参考设 置 反向方 向 文档
15
关于插入UDF的缺省设置
16
编辑一个UDF
编辑用户自定义特征的功能:
可以编辑插入的UDF的参数 可以对UDF进行重新定位 可以将UDF进行重新赋着 可以将UDF进行炸开,炸开时,将 自动创建一特征组
编辑插入的用户自定义特征的步骤:
在部件导航器中,选取用户自定义 特征,选取MB3 Edit Parameters 选取菜单Edit Feature Parameters
17
替换一用户自定义特征
替换用户自定义特征的步骤:
在部件导航器中,选取用户自定义特征,选取MB3 Feature 从用户自定义特征库中选取一新的用户自定义特征 在插入对话框中,给定正确的参数 通过匹配对话框,对对应几何进行正确的匹配 选取Apply完成。 Replace User Defined
18
5
用户自定义特征工具
Insert Tools File Design Feature User Defined …
插入已定义的用户自定义特征
User Defined Feature Export User Defined Feature
定义用户自定义特征,插入用户自定义特征 定义用户自定义特征
6
创建一个UDF
13
插入一个UDF
插入用户自定义特征到当前部件步骤:
用下列方式之一选取一UDF
Tools User Defined Feature Insert… Insert Design Feature User Defined 从用户自定义特征资源条中,拖拽一UDF到图形窗口
根据UDF创建窗口,给定参数、参考对象、放置层等 在某些情况下,参考匹配窗口将帮助确定选取对象之间的匹配问题。 在图形窗口中创建UDF 如果可能,将出现定位方式对话框帮助进行UDF定位
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Tutorial:Modeling Uniform Fluidization in2D Fluidized BedIntroductionThe prediction of pressure drop in an uniformlyfluidized bed is a problem of long standing interest in the process industry.The Eulerian models in ANSYS FLUENT provide an impor-tant modeling tool for studying dense phase particulateflow involving complex inter-phase momentum transfer.Despite rigorous mathematical modeling of the associated physics,the drag laws used in the model continue to be semi-empirical in nature.Therefore,it is crucial to use a drag law that correctly predicts the incipient or minimumfluidization conditions where the bed of particles is essentially in a state of suspension as a result of the balance between interfacial drag and body forces.The purpose of this tutorial is to study the hydrodynamics and bubble formation in a fluidized bed over a period of time.It also demonstrates how to customize a drag law for granular gas-solidflow.This tutorial demonstrates how to do the following:•Customize a drag law for granular gas-solidflow.•Use the Eulerian models to predict the pressure drop in an uniformlyfluidized bed.•Solve the case using appropriate solver settings.•Postprocess the resulting data.PrerequisitesThis tutorial is written with the assumption that you have completed Tutorial1from the ANSYS FLUENT12.0Tutorial Guide,and that you are familiar with the ANSYS FLUENT navigation pane and menu structure.Some steps in the setup and solution procedure will not be shown explicitly.This tutorial will not cover the mechanics of using the Eulerian models.It will focus on the application of these models.For more information refer to Section24.5Setting Up the Eulerian Model in the ANSYS FLUENT User’s Guide.For information about user-defined fucntions(UDF)refer to the ANSYS FLUENT UDF Manual.Modeling Uniform Fluidization in 2D Fluidized BedProblem DescriptionThe default drag law in ANSYS FLUENT is the Syamlal-O’Brien drag law.This law works for a large variety of problems,but has to be tuned properly for predicting the minimum fluidization conditions accurately.The default Syamlal-O’brien is as follows:The fluid-solid exchange coefficient isK sl =3αs αlρl 4v 2r,s d s C D Re sv r,s | v s − v l |where v 2r,sis the terminal velocity coefficient for the solid phase.v r,s =0.5 A −0.06Re s + (0.06Re s )2+0.12Re s (2B −A )+A 2with A =α4.14l and B =0.8α1.28l for αl ≤0.85and with B =α2.65lfor αl >0.85The default constants of 0.8and 2.65predict a minimum fluidization of 21cm/s.The experimentally observed minimum fluidization for this particular case is 8cm/s.Therefore,by changing the constants we can tune the drag law to predict minimum fluidization at 8cm/s.After some mathematical manipulation,these constants come out to be 0.281632and 9.07696respectively.Therefore,these values have to be used to predict the correct bed behavior and are passed to the code through user-defined functions.The problem considered is a 1m x 0.15m fluidized bed as shown in Figure 1.The inlet air enters in at 0.25m/s and the top is modeled as a pressure outlet.The bed is packed with granular solids at 0.55volume fraction (close topacking).Figure 1:Problem SpecificationModeling Uniform Fluidization in2D Fluidized Bed Preparation1.Copy thefiles,bp.msh.gz and bp drag.c to the working folder.e FLUENT Launcher to start the2D version of ANSYS FLUENT.For more information about FLUENT Launcher see Section1.1.2Starting ANSYS FLU-ENT Using FLUENT Launcher in the ANSYS FLUENT12.0User’s Guide.3.Enable Double-Precision in the Options list.4.Click the UDF Compiler tab and make sure that Setup Compilation Environment forUDF is enabled.The path to the.batfile which is required to compile the UDF will be displayed as soon as you enable Setup Compilation Environment for UDF.If the UDF Compiler tab does not appear in the FLUENT Launcher dialog box by default, click the Show Additional Options>>button to view the additional settings.Note:The Display Options are enabled by default.Therefore,after you read in the mesh,it will be displayed in the embedded graphics window.Setup and SolutionNote:All entries in setting up this case are in SI units,unless otherwise specified.Step1:Mesh1.Read the meshfile bp.msh.gz.File−→Read−→Mesh...Figure2:Graphics Display of the MeshModeling Uniform Fluidization in2D Fluidized BedStep2:General1.Check the mesh.−→CheckANSYS FLUENT will perform various checks on the mesh and will report the progressin the console.Ensure that the minimum volume reported is a positive number.2.Enable the transient solver by selecting Transient from the Time list.−→TransientStep3:Models1.Select the Eulerian multiphase model.−→−→Edit...(a)Select Eulerian from the Model selection list.(b)Retain the default settings and close the Multiphase Model dialog box.Step4:Materials1.Modify the properties for air.−→air−→Create/Edit...(a)Enter1.2kg/m3for Density.(b)Enter1.8e-05kg/m-s for Viscosity.(c)Click Change/Create.2.Define a material called solids.Modeling Uniform Fluidization in2D Fluidized Bed(a)Enter solids for Name.(b)Enter2600kg/m3for Density and1.7894e-05kg/m-s for Viscosity.(c)Click Change/Create.A Question dialog box will appear asking if you want to overwrite air.Click No.3.Close the Create/Edit Materials dialog box.Step5:Compile the UDFThe UDF contains two arguments s col and f col.These refer to the indices of the phases appearing in the second andfirst columns of the table in the interaction dialog box respec-tively.Therefore in this case s col refers to the index of gas phase which is0and f col refers to the index for solids which is equal to1.Define−→User-Defined−→Functions−→Compiled...1.Click the Add...button in the Source Files section to open the Select File dialog.2.Select thefile bp drag.c.3.Enter lib drag for Library Name.4.Click Build.A Warning dialog box will appear,warning you to make sure that the UDF sourcefilesare in the same folder that contains the case and datafiles.Click OK to close the Warning dialog box.You can view the compilation history in the logfile that is saved in your working folder.5.Click Load to load the library.Modeling Uniform Fluidization in2D Fluidized BedStep6:Phases1.Define primary phase.−→−→Edit...(a)Enter gas for Name.(b)Ensure air is selected from the Phase Material drop-down list.(c)Click OK to close the Primary Phase dialog box.2.Define secondary phase.−→−→Edit...Modeling Uniform Fluidization in2D Fluidized Bed(a)Enter solid for Name.(b)Select solids from the Phase Material drop-down list.(c)Enable Granular.(d)Enter0.0003m for Diameter,and select syamlal-obrien from the Granular Viscositydrop-down list.(e)Retain the default values for the other parameters.(f)Click OK to close the Secondary Phase dialog box.Check the column numbers where the two phases appear in the Phase Interaction dialog box.In this case solid and gas appear in thefirst and second columns respectively.These columns are used to specify the phase indices in the argument list for the UDF.3.Set the drag coefficient.(a)Select gas from the Phases selection list and click the Interaction...button toopen the Phase Interaction dialog box.i.Select user-defined from the drop-down list in the Drag Coefficient group box.Modeling Uniform Fluidization in2D Fluidized BedA.Ensure that custom drag syam::lib drag is selected.B.Click OK to close the User-Defined Functions dialog boxii.Click OK to close the Phase Interaction dialog box.(b)Similarly select the user defined function for solid(custom drag syam::lib drag).Step7:Boundary Conditions1.Set the boundary conditions for vinlet zone.−→(a)Select gas from the Phase drop-down list and click Edit....i.Select Components from the Velocity Specification Method drop-down list.ii.Enter0.25m/s for Y-Velocity.iii.Click OK to close the Velocity Inlet dialog box.(b)Select solid from the Phase drop-down list and click the Edit...button to openthe Velocity Inlet dialog box.i.Click the Multiphase tab.ii.Ensure that Volume Fraction is0.iii.Click OK to close the Velocity Inlet dialog box.Modeling Uniform Fluidization in2D Fluidized Bed Step8:Operating Conditions−→Operating Conditions...1.Enable Gravity and enter-9.81m/s2for Gravitational Acceleration in the Y direction.2.Enable Specified Operating Density,and enter1.2kg/m3for Operating Density.3.Click OK to close the Operating Conditions dialog box.Step9:Solution1.Mark a region for adaption.Adapt−→Region...Modeling Uniform Fluidization in2D Fluidized Bed(a)Enter0.15m for X Max and Y Max respectively in the Input Coordinates groupbox.(b)Click Mark to mark the cells for refinement.Note:Click Adapt to perform the refinement immediately.(c)Close the Region Adaption dialog box.2.Set the solution control parameters.(a)Enter0.5for Pressure in the Under-Relaxation Factors group box.(b)Enter0.2for Momentum.(c)Enter0.4for Volume Fraction.3.Initialize theflow with default values.−→Initialize4.Patch the solids volume fraction for hexahedron-r0.−→Patch...(a)Select solid from the Phase drop-down list.(b)Select Volume Fraction from the Variable selection list.(c)Enter0.55for Value.(d)Select hexahedron-r0from the Registers to Patch selection list.If you wish to patch a constant value,enter that value in the Valuefield.If you want to patch a previously-definedfield function,enablethe Use Field Function option and select the appropriate function inthe Field Function list.(e)Click Patch and close the Patch dialog box.5.Enable autosaving of the datafiles for every100time steps.Activities(a)Enter100for Autosave Every(Time Steps).6.Set up commands for animation.Activities(Execute Commands)−→Create/Edit...(a)Set2for Defined Commands.(b)Enable Active for both commands.(c)Set10for Every for both commands.(d)Select Time Step from the When drop-down list for both.(e)Enter/display/contour/solid/vof for command-1.(f)Enter/display/hardcopy"vof-solids-%t.tiff"for command-2.(g)Click OK to close the Execute Commands dialog box.7.Set the graphics hardcopy format.File−→Save Picture...(a)Select TIFF from the Format list.(b)Select Color from the Coloring list.(c)Click Apply and close the Save Picture dialog box.8.Set up the contours display.−→−→Set Up...(a)Enable Filled from the Options group box.(b)Select solid from the Phase drop-down list.(c)Select Phases...and Volume Fraction from the Contours of drop-down lists.(d)Click Display and close the Contours dialog box.9.Save the casefile(bp.cas.gz).File−→Write−→Case...10.Start the calculation..(a)Enter0.001sec for Time Step Size.(b)Enter1400for Number of Time Steps.(c)Enable Extrapolate Variables.(d)Click Calculate.11.Save the datafile(bp.dat.gz).File−→Write−→Data...Step10:Postprocessing1.Display contours of volume fraction.(a)Read the datafile for the200th time step(bp-1-00200.dat).File−→Read−→Data...(b)Displayfilled contours of volume fraction for solid,at0.2sec(Figure3).−→−→Set Up...Figure3:Contours of Volume Fraction of solid(t=0.2s)(c)Similarly display contours at0.9sec(Figure4),and1.4sec(Figure5).Figure4:Contours of Volume Fraction of solid(t=0.9s)Figure5:Contours of Volume Fraction of solid(t=1.4s)2.View the animation for thefluidization process using the.tifffiles.ResultsTypically,the constants set to0.8and2.65in the default drag law have to be modified to balance the interfacial drag with the weight of the bed at minimumfluidization.If this is not done,the correct bubbling pattern will not be predicted,leading to incorrect predictionsof pressure drop which is the most important objective of such simulations.。

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