ansys求解后处理过程
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2009-04-28 14:26ANSYS中查看截面结果的方法一般情况下,对计算结果后处理时,显示得到的云图为结构的外表面信息。
有时候,需要查看结构内部的某些截面云图,这就需要通过各种后处理技巧来获得截面的结果云图。
另外,有时候需要获得截面的结果数据,也需要用到后处理的技巧。
下面对常用的查看截面结果的方法做一个介绍:1. 通过工作平面切片查看截面云图工作平面实现。
这是比较常用的一种方法。
首先确保已经求解了问题,并得到了求解结果。
调整工作平面到需要观察的截面,可通过移动或者旋转工作平面实现。
调整时注意保证工作平面与需要观察的截面平行。
在PlotCtrls菜单中设置观察类型为Section,切片平面为Working Plane。
也可以通过等效的/type以及/cplane命令设置。
在通用后处理器中显示云图,得到需要查看的云图。
更简单地说,我们只需在显示云图命令前加上下面两条命令就可以了:/CPLANE,1 ! 指定截面为WP/TYPE,1,5 ! 结果显示方式选项2. 通过定义截面查看截面云图这种方法也需要用到工作平面与切片,步骤如下:首先确保已经得到了求解结果。
调整工作平面到需要观察的截面。
在PlotCtrls菜单中设置观察类型为Working Plane,或者使用命令/cplane,1。
通过sucr命令定义截面,选择(cplane)。
通过sumap命令定义需要查看的物理量。
通过supl命令显示结果。
3. 通过定义路径查看云图与保存数据首先确保已经得到了求解结果。
通过path与ppath命令定义截面路径。
通过pdef命令映射路径。
通过plpath、prpath与plpagm命令显示及输出结果。
总结:第一种方法是较简单、较常用的方式。
通过这种操作方式,我们也可以更直观地理解工作平面的含义。
以前看书上介绍工作平面总是无法理解到底什么是工作平面,工作平面有什么用途。
第二中方法实质上和第一种方法是一样的,只不过截面是我们自定义的一个平面,不是通过移动、旋转工作平面来实现“切片”的。
一、显示某个时间点的温度云图1、General Postproc →Read Result →By Time/Freq2、在跳出的窗口中输入时间点,点击OK按钮3、然后点Plot Results按下图操作3、然后点击plot →Replot即可显示该时刻的云图二、提取某个节点的数值1、首先通过下列命令,选择部分单元nsel,s,loc,x,0,0.025esln,all然后读取所需节点的编号。
2、点击时间历程后处理器TimeHist postproc弹出如箭头所指对话框。
点击图对话框左上角的绿色增加按钮弹出对话框点击ok按钮,在弹出的对话框中输入节点编号,或者鼠标点击选择节点即可将新的数据读入对话框中如下图所示然后即可通过窗口上的按钮对数据进行操作处理。
/POST1set,last !定义数据集从结果文件中读出,last表示读取最后的数据集plnsol,s,eqv !以连续的轮廓线形式显示结果,S表示应力,EQV表示等效应力查看某个截面的云图!-----------------选取节点结果/post1!seltol,1.0e-10set,,,,,2.5!nsel,s,loc,y,0.1,0.1nsel,s,loc,x,0.02/page,99999,132,99999,240!-------------------显示某个截面wprota,,,90wpoffs,,,0.02/CPLANE,1 !指定截面为WP/TYPE,1,5 !结果显示方式选项工作平面移回全局坐标原点WPCSYS,-1nsel,s,loc,x,0,0.025esln,,1,ACTIVE。
一、显示某个时间点的温度云图1、General Postproc →Read Result →By Time/Freq2、在跳出的窗口中输入时间点,点击OK按钮3、然后点Plot Results按下图操作3、然后点击plot →Replot即可显示该时刻的云图二、提取某个节点的数值1、首先通过下列命令,选择部分单元nsel,s,loc,x,0,0.025esln,all然后读取所需节点的编号。
2、点击时间历程后处理器TimeHist postproc弹出如箭头所指对话框。
点击图对话框左上角的绿色增加按钮弹出对话框点击ok按钮,在弹出的对话框中输入节点编号,或者鼠标点击选择节点即可将新的数据读入对话框中如下图所示然后即可通过窗口上的按钮对数据进行操作处理。
/POST1set,last !定义数据集从结果文件中读出,last表示读取最后的数据集plnsol,s,eqv !以连续的轮廓线形式显示结果,S表示应力,EQV表示等效应力查看某个截面的云图!-----------------选取节点结果/post1!seltol,1.0e-10set,,,,,2.5!nsel,s,loc,y,0.1,0.1nsel,s,loc,x,0.02/page,99999,132,99999,240!-------------------显示某个截面wprota,,,90wpoffs,,,0.02/CPLANE,1 !指定截面为WP/TYPE,1,5 !结果显示方式选项工作平面移回全局坐标原点WPCSYS,-1nsel,s,loc,x,0,0.025esln,,1,ACTIVE。
ansys命令流--前后处理和求解常用命令之求解与后处理any命令流----前后处理和求解常用命令之求解与后处理.t某t都是一个山的狐狸,你跟我讲什么聊斋,站在离你最近的地方,眺望你对别人的微笑,即使心是百般的疼痛只为把你的一举一动尽收眼底.刺眼的白色,让我明白什么是纯粹的伤害。
3/oluu/olu进入求解器3.1加边界条件uD,node,lab,value,value2,nend,ninc,lab2,lab3,lab6定义节点位移约束Node:预加位移约束的节点号,如果为all,则所有选中节点全加约束,此时忽略nend和ninc.Lab:u某,uy,uz,rot某,roty,rotz,allValue,value2:自由度的数值(缺省为0)3.2设置求解选项uantype,tatu,ldtep,ubtep,actionantype:taticor1静力分析buckleor2屈曲分析modalor3模态分析tranor4瞬态分析tatu:new重新分析(缺省),以后各项将忽略ret再分析,仅对tatic,fulltranion有效ldtep:指定从哪个荷载步开始继续分析,缺省为最大的,runn数(指分析点的最后一步)ubtep:指定从哪个子步开始继续分析。
缺省为本目录中,runn文件中最高的子步数action,continue:继续分析指定的ldtep,ubtep说明:继续以前的分析(因某种原因中断)有两种类型ingleframeretart:从停止点继续需要文件:jobname.db必须在初始求解后马上存盘jobname.emat单元矩阵jobname.eav或.oav:如果.eav坏了,将.oav改为.eavreultfile:不必要,但如果有,后继分析的结果也将很好地附加到它后面注意:如果初始分析生成了.rdb,.ldhi,或rnnn文件。
必须删除再做后继分析步骤:(1)进入anay以同样工作名(2)进入求解器,并恢复数据库(3)antype,ret(4)指定附加的荷载(5)指定是否使用现有的矩阵(jobname.trl)(缺省重新生成)kue:1用现有矩阵(6)求解multiframeretart:从以有结果的任一步继续(用不着)upred,key,--,lkey..在非线性分析中是否打开预测器key:off不作预测(当有旋转自由度时或使用olid65时缺省为off)on第一个子步后作预测(除非有旋转自由度时或使用olid65时缺省为on)--:未使用变量区lkey:off跨越荷载步时不作预测(缺省)on跨越荷载步时作预测(此时key必须同时on)注意:此命令的缺省值假定olcontrol为onuautot,key是否使用自动时间步长key:on:当olcontrol为on时缺省为onoff:当olcontrol为off时缺省为off 1:由程序选择(当olcontrol为on且不发生autot命令时在.log文件中纪录“1”注意:当使用自动时间步长时,也会使用步长预测器和二分步长uNROPT,option,--,adptky指定牛顿拉夫逊法求解的选项OPTION:AUTO:程序选择FULL:完全牛顿拉夫逊法MODI:修正的牛顿拉夫逊法INIT:使用初始刚阵UNSYM:完全牛顿拉夫逊法,且允许非对称刚阵ADPTKY:ON:使用自适应下降因子OFF:不使用自适应下降因子uNLGEOM,KEYKEY:OFF:不包括几何非线性(缺省)ON:包括几何非线性uncnv,ktop,dlim,itlim,etlim,cplim终止分析选项ktop:0如果求解不收敛,也不终止分析1如果求解不收敛,终止分析和程序(缺省)2如果求解不收敛,终止分析,但不终止程序dlim:最大位移限制,缺省为1.0e6itlim:累积迭代次数限制,缺省为无穷多etlim:程序执行时间(秒)限制,缺省为无穷cplim:cpu时间(秒)限制,缺省为无穷uolcontrol,key1,key2,key3,vtol指定是否使用一些非线性求解缺省值key1:on激活一些优化缺省值(缺省)CNVTOLToler=0.5%Minref=0.01(对力和弯矩)NEQIT最大迭代次数根据模型设定在15~26之间ARCLEN如用弧长法则用较any5.3更先进的方法PRED除非有rot某,y,z或olid65,否则打开LNSRCH当有接触时自动打开CUTCONTROLPllimit=15%,npoint=13SSTIF当NLGEOM,on时则打开NROPT,adaptkey关闭(除非:摩擦接触存在;单元12,26,48,49,52存在;当塑性存在且有单元20,23,24,60存在)AUTOS由程序选择off不使用这些缺省值key2:on检查接触状态(此时key1为on)此时时间步会以单元的接触状态(据keyopt(7)的假定)为基础当keyopt(2)=on时,保证时间步足够小key3:应力荷载刚化控制,尽量使用缺省值空:缺省,对某些单元包括应力荷载刚化,对某些不包括(查)nopl:对任何单元不包括应力刚化incp:对某些单元包括应力荷载刚化(查)vtol:uoutre,item,freq,cname规定写入数据库的求解信息item:all所有求解项baic只写nol,rol,nload,trnol节点自由度rol节点作用荷载nload节点荷载和输入的应变荷载(?)tr节点应力freq:如果为n,则每n步(包括最后一步)写入一次none:则在此荷载步中不写次项all:每一步都写lat:只写最后一步(静力或瞬态时为缺省)3.3定义载荷步unubt,nbtp,nbm某,nbmn,carry指定此荷载步的子步数nbtp:此荷载步的子步数uf,node,lab,value,value2,nend,ninc在指定节点加集中荷载node:节点号lab:F某,Fy,Fz,M某,My,Mzvalue:力大小value2:力的第二个大小(如果有复数荷载)nend,ninc:在从node到nend的节点(增量为ninc)上施加同样的力注意:(1)节点力在节点坐标系中定义,其正负与节点坐标轴正向一致ufa,area,lkey,lab,value,value2在指定面上加荷载area:n面号all 所有选中号lkey:如果是体的面,忽略此项lab:prevalue:压力值uSFBEAM,ELEM,LKEY,LAB,VALI,VALJ,VAL2I,VAL2J,IOFFST,JOFFST对梁单元施加线荷载ELEM:单元号,可以为ALL,即选中单元LKEY:面载类型号,见单元介绍。
ANSYS后处理1.ANSYS后处理时如何按灰度输出云图?1)你可以到utilitymenu-plotctrls-style-colors-window colors试试2)直接utilitymenu-plotctrls-redirect plots2 将云图输出为JPG菜单->PlotCtrls->Redirect Plots->To JPEG Files3.怎么在计算结果实体云图中切面?命令流/cplane/type图形界面操作<1.设置工作面为切面<2.PlotCtrls-->Style-->Hidden line Options将[/TYPE]选项选为section将[/CPLANE]选项选为working plane4.非线性计算过程中收敛曲线实时显示solution>load step opts>output ctrls>grph solu track>on5.运用命令流进行计算时,一个良好的习惯是:使用SELECT COMMEND后.........其后再加上ALLSEL.........6.应力图中左侧的文字中,SMX与SMN分别代表最大值和最小值如你plnsolv,s,eqv则 SMX与SMN分别代表最大值等效应力和最小值等效应力如你要看的是plnsolv,u则SMX与SMN分别代表位移最大值和位移最小值不要被S迷惑mx(max)mn(min)7.在非线性分析中,如何根据ansys的跟踪显示来判断收敛?在ansys output windows 有 force convergence value值和 criterion 值当前者小于后者时,就完成一次收敛你自己可以查看两条线的意思分别是:FL2:不平衡力的2范数 FCRIT:不平衡力的收敛容差,如果前者大于后者说明没有收敛,要继续计算,当然如果你以弯矩M为收敛准则那么就对应 M L2 和 M CRIT希望你现在能明白8.两个单元建成公共节点,就成了刚性连接,不是接触问题了。
第7章ANSYS命令:解题与后处理Solution and Postprocessing本章介绍solution模块(/SOLU)及两个postprocessing模块(/POST1及/POST26)中所使用到的命令。
在solution模块中,我们把命令分成三类(Figure 5-2):指定loads、指定solution options,及执行solve的命令。
本章第1节介绍前一类,后两类则在第2节介绍。
第3节介绍general postprocessing(/POST1)的命令。
第4节则介绍time-history postprocessing(/POST26)的命令。
最后,第5节以一个综合性的练习题作为本章的结束。
第7.1节负载Loads前面提过[Sec. 5.1.2] loads可以指定在analysis model(即nodes、elements)上,或指定loads在solid model(即keypoints、lines、areas、volumes)上。
除此之外,针对动态的问题,必须指定initial conditions,亦即初始时间的边界条件。
这一节分别介绍loads on analysis model [Sec. 7.1.1]、loads on solid model [Sec. 7.1.2]、及initial conditions [Sec. 7.1.3] 的命令。
Loads虽然可以指定在solid model上,但是「解题」的对象是analysis model,所以那些指定在solid model上的loads终究必须「移转」(transfer)到analysis model上。
这种移转的工作可以让ANSYS自动去完成:ANSYS会在解题前先做负载移转的工作。
或者你也可以在解题之前利用诸如SBCTRAN [Sec. 7.1.2] 的命令去移转这些负载,因为有时侯你希望在解题之前自己检视一下analysis model 上的loads是否正确。
ansys命令流----前后处理和求解常用命令之求解与后处理The ANSYS command stream - before and after the treatment and solving common commands of solving and postprocessing of.Txt is a mountain fox, you told me what all, standing in the place nearest to you, look you smile to others, even if the heart is all the pain just to keep your eye out. The glare of the bottom of every act and every move white, let me understand what is pure damage. 3 /soluU /solu enters the solver3.1 plus boundary conditionsU, D, node, lab, value, Value2, nend, Ninc, lab2, lab3,...... LaB6 defines node displacement constraintsNode: the node number of the pre displacement constraint. If it is all, all selected nodes are fully bound, and nend and ninc. are ignored at this timeLab:, UX, uy, UZ, ROTx, ROTY, Rotz, allThe value of Value, value2: degrees of freedom (default 0)Nend, ninc: node range is: node-nend, the number interval is NincLab2-lab6: applies lab2-lab6 to the selected node with the same value.Note: discussed in the node coordinate system3.2 set the solution optionU, antype, status, ldstep, substep, actionStatic analysis of antype:, static and or 1Buckling analysis of buckle or 2Modal or 3 modal analysisTransient analysis of trans or 4Status: new reanalysis (default), which will be ignored later Rest reanalysis is valid only for static, full, and transionLdstep: specifies which load step to proceed from the analysis and defaults to the maximum runn number (the last step of the analysis point)Substep: specifies which sub step to proceed from the analysis. The default is the highest number of sub steps in the runn file in this directoryAction, continue: continues to analyze the specified ldstep, substepExplanation: there are two types of continuous analysis (interrupted for some reason)Singleframe restart: continues from the stop pointRequired file: jobname.db must be saved immediately after initial solutionJobname.emat cell matrixJobname.esav or.Osav: if.Esav is broken, change.Osav to.EsavResults file: is not necessary, but if so, the results of subsequent analysis will be well attached to itNote: if the initial analysis generates a.Rdb,.Ldhi, or rnnn file. Deletion must be followed by subsequent analysisStep: (1) enter ANASYS with the same job name(2) enter the solver and restore the database(3) antype, rest(4) additional load is specified(5) specify whether to use the existing matrix (jobname.trl) (default rebuild)Kuse: 1 uses an existing matrix(6) solvingMultiframe restart: continues from any result with no result(no need)U, PRED, sskey -- -- lskey... Whether to open the predictor in nonlinear analysisSskey: off does not make predictions (when the degree of freedom is rotated or when SOLID65 is used, default is off)The first step was to predict on (unless there is a rotational degree of freedom or when using the SOLID65 default is on)- - unused variable zoneLskey: off does not predict when crossing load steps (default)On predicts when crossing load steps (at this time sskey must be simultaneous on)Note: the default value for this command assumes that solcontrol is onDoes u autots and key use automatic time steps?Key:on: when solcontrol is on, the default is onOff: when solcontrol is off, the default is off1: records in the.Log file "1" by the program selection (when solcontrol is on and does not occur the autots command"Note: the step size predictor and the two step size are alsoused when using the automatic time stepU, NROPT, option -- -- adptky specifies the options for Newton Ralph Xun Fa's solutionOPTION: AUTO: program selectionFULL: completely Newton Ralph Xun FaMODI: revised by Newton Ralph Xun FaINIT: using the initial stiffness matrixUNSYM: complete Newton Ralph Xun Fa, and allows asymmetric stiffness matricesADPTKY:ON: uses adaptive drop factorOFF: no adaptive drop factor is usedU, NLGEOM, KEYKEY: OFF: does not include geometric nonlinearity (default)ON: including geometric nonlinearityU, ncnv, kstop, dlim, itlim, etlim, cplim, terminate the analysis optionsKstop: 0, if the solution is not convergent, does not terminate the analysis1 if the solution does not converge, terminate the analysis and the program (default)2 if the solution does not converge, terminate the analysis, but do not terminate the programDlim: maximum displacement limit, defaults to 1.0e6Itlim: cumulative iteration limit, default to infinityEtlim: program execution time (seconds) limit, the default is infiniteCplim:cpu time (seconds) limit, default to infinityThe U, solcontrol, key1, key2, Key3, and VTOL specify whether or not to use some nonlinear solutions for default valuesKey1: on activates some optimized default values (default)CNVTOL, Toler=0.5%Minref=0.01 (for force and moment)NEQIT the maximum number of iterations is set between 15~26 depending on the modelARCLEN uses the more advanced method of ansys5.3 than using the arc length rulePRED unless ROTx, y, Z, or SOLID65 are openedLNSRCH automatically opens when exposedCUTCONTROL, Plslimit=15%, npoint=13SSTIF opens when NLGEOM, onNROPT, adaptkey closes (unless the frictional contact exists; the unit 12,26,48,49,52 exists; when the plastic is present and there is a unit 20,23,24,60)AUTOS is chosen by the programOff does not use these default valuesKey2: on checks the contact state (key1 at on)At this point, the time step is based on the contact state of the unit (assuming keyopt (7))When keyopt (2) =on, the time step is guaranteed to be small enoughKey3: stress loading stiffness control, use default values as much as possibleNull: by default, certain units include stress loading, stiffening, and certain ones (excluding)Nopl: does not include stress stiffening for any elementIncp: for some elements including stress load stiffening(check)Vtol:U, outres, item, freq, and CNAME specify the solution information for writing to the databaseItem: all all the solutionsBasic only writes nsol, rsol, nload, STRsNsol node freedomRsol node acting loadNload nodal loads and input strain loads (?)STRs node stressIf n is freq:, it is written once every n step (including the last step)None: does not write entries in this load stepAll: writes every stepLast: writes only the last step (default when static or transient)3.3 define the load stepThe U, nsubst, nsbstp, nsbmx, nsbmn, and carry specify the number of sub steps for this load stepNsbstp: the number of sub steps of this load stepIf automatic time step using autots, the number of the first definition step length; if solcontrol is open, and 3D surface to surface contact element is used, the default is 1-20; if solcontrol is open, there is no 3D contact element, the default is 1 steps; if the solcontrol is closed, the default value is specified as before; not previously specified, the default is 1)Nsbmx, nsbmn: at most, the minimum number of steps (if the automatic time step is turned on)?U time, time specifies the end time of the load stepNote: the end of the first step shall not be "0""U F, node, lab, Ninc, value, Value2, nend, plus concentrated load at the specified nodeNode: node numberLab:, Fx, Fy, Fz, Mx, My, MzValue: force sizeThe second magnitude of the force of value2: (if there is a complex load)Nend, Ninc: apply the same force on the node from node to nend (increment Ninc)Note: (1) the nodal force is defined in the nodal coordinate system, and the positive and negative forces are in direct agreement with the nodal coordinate axisU, SFA, area, lkey, lab, value, and Value2 add loads on the specified surfaceArea: n surface numberAll all selected numbersLkey: if it is the surface of the body, ignore this itemLab: presValue: pressure valueU, SFBEAM, ELEM, LKEY, LAB, VALI, VALJ, VAL2I, VAL2J, IOFFST, JOFFSTApply line load to the beam elementThe ELEM: cell number can be ALL, that is, the selected cellLKEY: surface mounted type number, see unit introduction. For BEAM188, 1 is vertical; 2 is transverse; 3 is tangentialPressure values at VALI, VALJ:, I, and J nodesVAL2I, VAL2J: is useless for the momentIOFFST, JOFFST:, line distance, I, J node distanceU, lswrite, lsnum write the load and load options into the load fileLsnum: the suffix of the load step file name, that is, the number of loading stepsWhen the stat column shows the current step numberInit reset to "1""The default is to add 1 to the current step"3.3.1 attention1. add as much load as possible without focusing so as to avoid singularitiesThe tangential load on the 2. plane must depend on the surface element3.4 load stepsU, lssolve, lsmin, lsmax, lsinc read and solve multiple loading stepsLsmin, lsmax, lsinc: load step file range4 /post1 (general postprocessing)U, set, lstep, sbstep, fact, king, time, angle, and nset set the data read from the result fileLstep: load stepsSbstep: child steps and defaults to the last stepTime: point of time (if the arc length rule does not)Nset:data set numberU, dscale, WN, dmult display deformation ratioWn: window number (or all), defaults to 1Dmult, 0 or Auto: automatically make the maximum deformation picture 5% of the length of the componentU, pldisp, and Kund display the structure of deformationKund:0 only shows the structure after deformation1 shows the structure before deformation and after deformation2 shows the deformation structure and the edge of the undeformed structureU, *get, par, node, N, u, X (y, z) obtain the X (y, z) shift of node n to parameter parEquivalent to the function UX (n), uy (n), UZ (z)Node (x, y, z): get the (x, y, z) node numberArnode (x, y, z): get the surface connected to the node nNote: this command can also be used with the /solu moduleU, fsum, lab, item, summation of nodal forces and moments of a unitLab: empty sum in the whole DeCarr coordinate systemRsys sums up in the current active rsys coordinate systemItem: empty sum for all selected units (not including contact elements)Cont: only sum the contact nodesU, PRSSOL, ITEM, COMP, print BEAM188, BEAM189 cross section resultsDescription: only when the calculation has not yet exited the ANSYS can be used and re entered the ANSYS is not availableItem comp cross section data and component markStress components of S, COMP, X, XZ and YZPRIN, S1, S2, S3, principal stress, SINT stress intensity, and SEQV equivalent stressEPTO COMP total strainPRIN total principal strain, strain strength and equivalent strainEPPL COMP plastic strain componentPRIN principal plastic strain, plastic strain strength, and equivalent plastic strainU, plnsol, item, comp, Kund, fact draw nodes, resulting in a continuous contour lineItem: project (see table below)Comp: componentKund: 0 does not display an undeformed structure1 deformation and deformation overlap2 deformation contours and undeformed edgesFact:'s coefficient of proportionality for exposure to 2D displays defaults to 1Item comp discriptionU, x, y, Z, sum shiftRot, x, y, Z, sum cornersS, x, y, Z, XY, YZ, XZ stress components1, 2, 3 principal stressesInt, EQV stress, intensity, equivalent stressEPEO, x, y, Z, XY, YZ, XZ total displacement components 1,2,3 principal strainInt, EQV strain, intensity, equivalent strainEPEL, x, y, Z, XY, YZ, and XZ elastic strain components 1, 2, 3 elastic principal strainInt, EQV, elastic intensity, elastic equivalent strain EPPL, x, y, Z, XY, YZ, XZ plastic strain componentsU PRNSOL, item, comp print select the node results Item: project (see above)Comp: componentU, PRETAB, LAB1, LAB2,...... Plotting unit table data along the length of units along LAB9LABn: null: column names specified by all ETABLE commandsColumn name: the column name specified by any ETABLE commandU, PLLS, LABI, LABJ, FACT, KUND, drawing unit table data along the unit length directionUnit table name of LABI: node IUnit table name of LABJ: node JFACT: display scale, default to 1Kund: 0 does not display an undeformed structure1 deformation and deformation overlap2 deformation contours and undeformed edges5 /post26 (time course postprocessing)U, nsol, NVAR, node, item, comp, nameIn the time course, the ordinal number of the node variable is defined in the processorNVAR: variable number (from 2 to NV (defined by numvar))Node: node numberItem compU, x, y, ZRot, x, y, ZU, ESOL, NVAR, ELEM, NODE, ITEM, COMP, and NAME store the results into variablesNVAR: variable number, more than 2ELEM: unit numberNODE: the node number of the unit determines which amount to store the unit and, if empty, gives the average valueITEM:COMP:NAME: 8 character variable name, defaults to ITEM plus COMPU, rforce, NVAR, node, item, comp, and name specify the node force data to be storedNvar: variable numberNode: node numberItem compF, x, y.zM, x, y, ZName: gives this variable a name, 8 charactersU, add, IR, IA, IB, IC, name, - - - -, facta, factb, factc Add the IA, IB, and IC variables to the IR variableIR, IA, IB, IC: variable numberThe name of the name: variableU, /grid, keyKey: "0" or "off" without network"1" or "on" XY network"2" or "X" is only X-ray"3" or "Y" has only y linesU, xvar, nN: "0" or "1" takes the X axis as the time axis"N" represents the X axis variable "n"""-1"?U, /axlab, axis, lab define the axis of the markAxis: "X" or "Y""The lab: flag can be up to 30 characters longU, plvar, NVAR, nvar2,...... Nvar10 draws the variable to be displayed (as a ordinate)U, prvar, nvar1,...... Nvar6 lists the variables to display6 PLOTCONTROL menu commandU, PBC, ilem,...... The key, min, Max, and ABS display symbols and values on the displayThe displacement constraint added by item: uRot corner constraintKey: 0 does not display symbols1 display symbols2 display symbols and valuesThe U, /SHOW, FNAME, EXT, VECT, and NCPL determine the graphicaldisplay of the device and other parametersFNAME: X11: screenFile name: each graphic will generate a series of graphic filesEach of the JPEG: graphics generates a series of JPEG graphics filesDescription: there is no need to use this command, graphics files need to be calculated and then output7 parametric design languageU, *do, par, ival, Fval, and inc define the beginning of a do loopPar: loop control variablesIval, Fval, Inc: start value, final value, step size (positive, negative)U *enddo defines the end of a do loopU, *if, val1, oper, val2, base: conditional statementsVal1 (val2:), the value to be compared (also characters, enclosed in quotes)Oper: logical operation (when the real number is compared, the error is 1e-10)EQ, NE, lt, GT, Le, Ge, ablt, abgtBase: behavior when the oper result is a logical truthLable: user defined line labelsStop: will jump out of ANASYSExit: jumps out of the current do loopCycle: jumps to the end of the current do loopThen: makes up the If-Then-Else structureNote: not allowed to jump out of, jump into a do, if loop to label sentence8 theoretical manualSolution of 1. equations: (1) direct solution; (2) iterative solution(1) direct solution: A. sparse matrix method and B. wave front methodA. sparse matrix method: accounting for large memory, but the number of operations less; by changing the order of stiffness matrix, so that non-zero elements minimumB. wavefront method: small memoryWavefront is the number of equations activated when no cell has been solved(2) iterative solution: JCG method, PCG method, ICCG methodJCG method: solvable real numbers, symmetric and unsymmetric matricesPCG method: efficient solution of various matrices (including morbid state), but only the real and symmetric matrixICCG: similar to JCG, but stronger2. strain density, equivalent strain, stress density, equivalent stress(1) strain density (strain, intensity);Strain densityAre the three principal strains(2) equivalent strainEffective Poisson's ratio: the user is set by the avprin command;0 (if not set)(3) stress density (stress, intensity);Stress density(4) equivalent stressEquivalent stress or if there is (elastic state)。
Workbench -Mechanical Introduction Introduction作业8.181结果后处理作业8.1 –目标Workshop Supplement •本作业分析了一个高压排气组件的应力和挠度。
•如果在结果后处理(postprocessing)中所有部件都激活的话,部分分析结果很难得到解释。
我们的目标是分离模型的部件,使用先进的结果很难得到解释我们的标是分离模型的部件使用先进的Workbench-Mechanical特性进行结果后处理。
作业8.1 –假设Workshop Supplement •假设:气体是由进气管到膨胀室被排出的。
在膨胀室内部,压力比进气管处降低了20%。
•膨胀室是刚性连接在进气管上的,因此把这里的接触定义为bonded。
膨胀室是刚性连接在进气管上的因此把这里的接触定义为•支架允许管子出现有限的移动,因此这里使用无分离接触。
查看下页的接触描述–查看下一页的接触描述•用结构钢(structural steel)模拟进气管和支架,而膨胀室是橡胶(Polyethylene)。
Workshop Supplement作业8.1 –部件和接触描述Expansion Bonded ContactChamber (膨胀室)(结合接触)Support Bracket (支架)No Separation Contact (无分离接触)Inlet Pipe Inlet Pipe (进气管)作业8.1 –Project SchematicWorkshop Supplement •打开Project 页•在Units 菜单中确定:–项目单位设为Metric (kg, mm, s, C, mA, mV)–选择Display Values in Project UnitsWorkshop Supplement… 作业8.1 –Project Schematic1.在Toolbox 中双击Static Structural创建一个新系统1.2.双击Engineering Data 得到material properties.p p3在General Materials 2.3.General Materials 中点击Polyethylene 旁的‘+’符号,把材料添加到当前系统3.Workshop Supplement. . . 作业8.1 –Project Schematic4.Return to Project (返回到项目)45在geometry 4.5.geometry 上点击鼠标右键选择Import Geometry ,导入文件Pressure_System.x_t5.6.双击Model Mechanical打开application6.Workshop Supplement作业8.1 –前处理7.设置作业单位制系统:•Units > Metric (mm, kg, N, s, mV, mA)8.改变expansion chamber 的材料:7.a.选中该膨胀室部分b.在details of solid 窗口中点击material 栏,改变material assignment material assignment为Polyethylene a.b.. . .作业8.1 –前处理Workshop Supplement9.根据管的接触行为修整支架:a.选中Connections下的Contact Region 2b.在Details of Contact Region 2窗口改变接触类型为No Separationa.b.Workshop Supplement作业8.1 –环境10.给管道施加一个压力:a.选中Static Structural (A5)b.选择管道的5个内表面(提示:使用Extend tolimits )c.RMB (点击鼠标右键选择)> Insert > P a.Pressured.输入Magnitude 值1MPab.c.d.. . .作业8.1 –环境Workshop Supplement11.给expansion chamber施加一个压力:a.选择expansion chamber的三个内表面提示使用平面选择状态栏和键可以简化选择•提示:使用平面选择,状态栏和CTRL键可以简化选择。
ANSYS 实体模型加载、求解及后处理步骤计算温度场步骤:1.定义标题和工作文件名1)定义标题:Utility Menu>Change Title2)定义工作文件名: Utility Menu>Change Jobname2.选择单元类型Main Menu>Proprecessor>Element Type>Add/Edit/Delete 出现一个“ Element Type”对话框,点击“ Add”,又出现一个“ Library of Element Type”对话框,选择“ Thermal Solid”,在右面的栏中选择“ Brick 20Node 90” ,单击“ OK ”。
3.定义材料属性1)设置材料密度 Main Menu>Proprecessor>Material Props>Material Models 出现一个“ Define Material Mode Behavior ”对话框,在右面的对话框中双击“ Thermal”,双击其下出现的“ Density”,出现“ Density for Material Number 1 ”的对话框,在“ DENS”后面输入密度值;2)输入导热系数 Main Menu>Proprecessor>Material Props>Material Models 出现一个“ Define Material Mode Behavior ”对话框,在右面的对话框中双击“ Thermal”,双击其下出现的“ Conductivity ”,双击“ Isotropic ”,出现一个“ Conductivity for Material Number 1”的对话框,连续单击“ Add Temperature”在“ KXX ”中输入导热系数值;3)定义比热在“ Define Material Mode Behavior”对话框右面输入栏中,双击“ Specific heat”,出现一个“ Specific heat for Material Number 1 ”对话框,连续单击“Add Temperature”,在“Temperature”中输入温度,在“C”中输入与温度对应的比热系数;4)输入对流系数在“ Define Material Mode Behavior”对话框右面输入栏中,双击“ Convection or Film Coef”,出现一个“ Convection or Film Coefficient for Material Number 1”对话框,在“ Temperature”中输入温度,在“ HF”后面输入与温度对应的对流数。