本文摘要（由AI生成）：本文展示了在ABAQUS中创建仿真模型、施加边界条件、集中力、重力、划分网格、创建作业并提交分析，以及进行后处理的过程。首先，通过定义边界条件和集中力来设置模型。然后，划分网格，并创建作业进行分析。分析完成后，通过后处理模块查看结果，并保存CAE文件。基于Python 的 Abaqus 的二次开发便捷之处在于：1、所有的代码均可以先在Abaqus CAE 中操作一遍后再通过 rp 文件读取，然后再在此基础上进行相应的修改；2、 Python 是一种解释性语言，读起来非常清晰，因此在修改程序的过程中，不存在程序难以理解的问题；3、 Python 是一种通用性的、功能非常强大的面向对象编程语言，有许多成熟的类似于Matlab 函数的程序在网络上流传，为后期进一步的数据处理提供了方便。为了更加方便地完成Abaqus 的二次开发，需进行一些相关约定：1、所有参数化直接通过点的坐标值进行，直接对几何尺寸的参数化反而更加繁琐2、程序参数化已不允许 在模型中添加太多的 Tie，因此不同零部件的绑定直接通过共节点来进行，这就要求建模方法与常规的建模方法有所区别。思路如下：将一个整机拆成几个大的Part 来建立，一个 Part 中包含许多零件，这样在划分网格式时 就可以自动实现共节点的绑定。不同的零件可通过建立不同的 Set 来进行区分，不同 Part 的绑定可以通过 Tie 来实现。将一个复杂的结构拆成几个 恰当的 Part 来建立，一方面可以将复杂的模型简单化，使建立复杂模型成为可能；另一方面，不同的 Part 可单独调用，从而又可实现程序的模块化，增加程序的适应范围，延长程序的使用寿命，也方便后期程序的维护和修改。3、通过py文件建立起的模型要进行参数优化已不适合采用 Isight 中 Abaqus 模块，需要用到 Isight 的 Simcode 模块 。下面详细解释一个臂架的 py 文件：#此程序用来绘制臂架前段#导入相关模块#coding: mbcsfrom abaqus import *from abaqusConstants import *#定义整个臂架的长、宽、高L0=14300W0=1650H0=800#创建零件P01_12L1=H0+200 W1=200 T1=12s = mdb.models['Model-1'].ConstrainedSketch(name=' profile ',sheetSize=2000.0)g, v, d, c = s.geometry, s.vertices, s.dimensions, s.constraints s.setPrimaryObject(option=STANDALONE) s.rectangle(point1=(W0/2, L1/2), point2=(W0/2+W1, -L1/2)) s.rectangle(point1=(-W0/2, L1/2), point2=(-W0/2-W1, -L1/2))p = mdb.models['Model-1'].Part(name='Part-1', dimensionality=THREE_D, type=DEFORMABLE_BODY)p = mdb.models['Model-1'].parts['Part-1'] p.BaseShell(sketch=s)session.viewports['Viewport: 1'].setValues(displayedObject=p) del mdb.models['Model-1'].sketches[' profile ']注：通过点的坐标进行参数化是模型参数化的 最 好选择。#定义零件的厚度p = mdb.models['Model-1'].parts['Part-1']f = p.facespickedFaces01 = f.findAt(((W0/2, L1/2, 0),),((-W0/2, L1/2, 0),), ) p.assignThickness(faces=pickedFaces01, thickness=T1)p.Set(faces=pickedFaces01, name='P01_12')注：建立一个零件后就立即对该零件建立一个 Set Set 的建立可以方便后期的相关处理。需要通过findAt() 命令来选取相应的体、面、线或点。#创建辅助平面和辅助坐标系p = mdb.models['Model1'].parts['Part 1']p.DatumCsysByThreePoints(name='Datum csys1', coordSysType=CARTESIAN, origin=(0.0, 0.0, 0.0), line1=(1.0, 0.0, 0.0), line2=(0.0, 1.0, 0.0))p = mdb.models['Model1'].parts['Part 1']p.DatumPlaneByPrincipalPlane(principalPlane=XYPLANE, offset=L0)注：所建立的第一个参考可以不编号。#创建零件P02_12L2=L1 W2=W1 T2=12p = mdb.models['Model-1'].parts['Part-1']d = p.datums#将草图原点参数化t = p.MakeSketchTransform(sketchPlane=d[5], sketchUpEdge=d[4].axis2, sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, origin=(0.0, 0.0, L0))s = mdb.models['Model-1'].ConstrainedSketch(name=' profile ', sheetSize=29006.85, gridSpacing=725.17, transform=t)g, v, d1, c = s.geometry, s.vertices, s.dimensions, s.constraints s.setPrimaryObject(option=SUPERIMPOSE)p = mdb.models['Model-1'].parts['Part-1']s.rectangle(point1=(W0/2, L2/2), point2=(W0/2+W2, -L2/2))s.rectangle(point1=(-W0/2, L2/2), point2=(-W0/2-W2, -L2/2)) p = mdb.models['Model-1'].parts['Part-1']d2 = p.datumsp.Shell(sketchPlane=d2[5], sketchUpEdge=d2[4].axis2, sketchPlaneSide=SIDE1,sketchOrientation=RIGHT, sketch=s)s.unsetPrimaryObject()del mdb.models['Model-1'].sketches[' profile ']注：从第二个草图开始就需要对草图的原点进行参数化。#定义零件的厚度p = mdb.models['Model1'].parts['Part 1']f = p.facespickedFaces02 = f.findAt(((W0/2, L1/2, L0),),((W0/2, L1/2, L0),), )p.assignThickness (faces=pickedFaces02, thickness=p.Set(faces=pickedFaces02, name='P02_12')注：给几何面赋厚度，可以在后期赋壳单元属性时直接选取几何面的厚度；也可以通过壳单元属性给建立的 Set 赋予厚度。两种方法适用于不同的情况。#创建零件 P03_12 和零件 P04_08T3=12T4=8p = mdb.models['Model1'].parts['Part 1']d = p.datumst = p.MakeSketchTransform(sketchPlane=d[5], sketchUpEdge=d[4].axis2,sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, origin=(0.0, 0.0, L0))s = mdb.models['Model1'].ConstrainedSketch(name='__profile__',sheetSize=29006.85, gridSpacing=725.17, transform=t)g, v, d1, c = s.geometry, s.vertices, s.dimensions, s.constraintss.setPrimaryObject(option=SUPERIMPOSE)#创建草图p = mdb.models['Model1'].parts['Part 1']s.Line(point1=(W0/2 W1, H0/2), point2=( W0/2, H0/2))s.Line(point1=(W0/2, H0/2), point2=(W0/2+W1, H0/2))s.Line(point1=(W0/2 W1, H0/2), point2=( W0/2, H0/2))s.Line(point1=(W0/2,H0/2), point2=(W0/2+W1, H0/2))p = mdb.models['Model1'].parts['Part 1']d2 = p.datumsp.ShellExtrude(sketchPlane=d2[5], sketchUpEdge=d2[4].axis2,sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, sketch=s, depth=L0,flipExtr udeDirection=ON)s.unsetPrimaryObject()del mdb.models['Model1'].sketches['__profile__']#定义零件 P03_12 的厚度p = mdb.models['Model1'].parts['Part 1']f = p.facespickedFaces03 = f.findAt(((W0/2, H0/2, L0/2),),((W0/2, H0/2, L0/2),),)p.assignThickness(faces=pickedFaces03, thickness=T3)p.Set(faces=pickedFaces03, name='P03_12')#定义零件P04_12 的厚度p = mdb.models['Model-1'].parts['Part-1'] f = p.facespickedFaces04 = f.findAt(((-W0/2, -H0/2, L0/2),),((W0/2, -H0/2, L0/2),),)p.assignThickness(faces=pickedFaces04, thickness=T4) p.Set(faces=pickedFaces04, name='P04_12')#创建零件P05_08 T5=8p = mdb.models['Model-1'].parts['Part-1'] d = p.datumst = p.MakeSketchTransform(sketchPlane=d[5], sketchUpEdge=d[4].axis2, sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, origin=(0.0, 0.0, L0))s = mdb.models['Model-1'].ConstrainedSketch(name=' profile ', sheetSize=29006.85, gridSpacing=725.17, transform=t)g, v, d1, c = s.geometry, s.vertices, s.dimensions, s.constraintss.setPrimaryObject(option=SUPERIMPOSE) p = mdb.models['Model-1'].parts['Part-1']s.Line(point1=(-W0/2-W1/2, H0/2), point2=(-W0/2-W1/2, -H0/2)) s.Line(point1=(W0/2+W1/2, H0/2), point2=(W0/2+W1/2, -H0/2)) p = mdb.models['Model-1'].parts['Part-1']d2 = p.datumsp.ShellExtrude(sketchPlane=d2[5], sketchUpEdge=d2[4].axis2, sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, sketch=s, depth=L0, flipExtrudeDirection=ON)s.unsetPrimaryObject()del mdb.models['Model-1'].sketches[' profile '] #定义零件P05_8 的厚度p = mdb.models['Model-1'].parts['Part-1']f = p.facespickedFaces05 = f.findAt(((-W0/2-W1/2, 0, L0/2),),((W0/2+W1/2, 0, L0/2),),)p.assignThickness(faces=pickedFaces05, thickness=T5) p.Set(faces=pickedFaces05, name='P05_08')#创建零件P06_08 L6=W0+W1 n=L0//2520+1T6=8p = mdb.models['Model-1'].parts['Part-1']f, d = p.faces, p.datumst = p.MakeSketchTransform(sketchPlane=f[0], sketchUpEdge=d[4].axis2, sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, origin=(W0/2+W1/2, -H0/2,0))s = mdb.models['Model1'].C onstrainedSketch(name='__profile__',sheetSize=28684, gridSpacing=717, transform=t)g, v, d1, c = s.geometry, s.vertices, s.dimensions, s.constraintss.setPrimaryObject(option=SUPERIMPOSE)p = mdb.models['Model1'].parts['Part 1']#循环命令绘制平行隔板for i in range(0,n):s.Line(point1=(-500-(i*2520), H0), point2=(-500-(i*2520), 0.0))p = mdb.models['Model-1'].parts['Part-1']f1, d2 = p.faces, p.datumsp.ShellExtrude(sketchPlane=f1[0], sketchUpEdge=d2[4].axis2, sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, sketch=s, depth=L6, flipExtrudeDirection=ON)s.unsetPrimaryObject()del mdb.models['Model-1'].sketches[' profile ']注：也可以将 range(0,n) 改成 自定义 数组，这样就可以实现不等间距的参数化控制。#定义零件P06_08 的厚度p = mdb.models['Model-1'].parts['Part-1'] f = p.facesfor i in range(0,n):pickedFaces = f.findAt(((0, H0/4, 500+i*2520),)) p.assignThickness(faces=pickedFaces, thickness=T6) p.Set(faces=pickedFaces, name='P06_08_'+str(1+i))注：将循环绘制的零件通过循环命令分别建立各自的 Set 并分别命名。也可以将循环绘制的零件建立成一个 Set ，视具体情况而定。#创建零件P07_12,P08_12W7=200 L7=W0+W1T7=12 T8=12p = mdb.models['Model-1'].parts['Part-1']f, e = p.faces, p.edgest = p.MakeSketchTransform(sketchPlane=f.findAt(coordinates=(W0/2+W1/2, 0.0, 100.0)),sketchUpEdge=e.findAt(coordinates=(W0/2+W1/2, 0.0, 0.0)), sketchOrientation=RIGHT,sketchPlaneSide=SIDE1, origin=(W0/2+W1/2, -H0/2, 0.0))s = mdb.models['Model-1'].ConstrainedSketch(name=' profile ', sheetSize=53678, gridSpacing=1341, transform=t)g, v, d, c = s.geometry, s.vertices, s.dimensions, s.constraintss.setPrimaryObject(option=SUPERIMPOSE) p = mdb.models['Model-1'].parts['Part-1'] #循环命令绘制平行隔板for i in range(0,n):s.Line(point1=(400+i*2520, -H0), point2=(600+i*2520, -H0))s.Line(point1=(400+i*2520, 0), point2=(600+i*2520, 0))p = mdb.models['Model-1'].parts['Part-1']f1, e1 = p.faces, p.edgesp.ShellExtrude(sketchPlane=f.findAt(coordinates=(W0/2+W1/2, 0.0, 100.0)),sketchUpEdge=e.findAt(coordinates=(W0/2+W1/2, 0.0, 0.0)), sketchPlaneSide=SIDE1,sketchOrientation=RIGHT, sketch=s, depth=W0+W1, flipExtrudeDirection=ON,keepInternalBoundaries=ON)s.unsetPrimaryObject()del mdb.models['Model-1'].sketches[' profile '] #定义零件P07_12 的厚度p = mdb.models['Model-1'].parts['Part-1'] f = p.facesfor i in range(0,n):pickedFaces07 = f.findAt(((0, H0/2, 400+i*2520),),((0, H0/2, 600+i*2520),),)p.assignThickness(faces=pickedFaces07, thickness=T7)p.Set(faces=pickedFaces07, name='P07_12_'+str(1+i))#定义耦合setfp=[]for i in range(0,2):fp.append(f.findAt(((0, H0/2, 400+i*2520),),((0, H0/2, 600+i*2520),),))p.Set(faces=fp, name='P07_fp') #定义零件P08_12 的厚度p = mdb.models['Model-1'].parts['Part-1'] f = p.facesfor i in range(0,n):pickedFaces08 = f.findAt(((0, -H0/2, 400+i*2520),),((0, -H0/2, 600+i*2520),),)p.assignThickness(faces=pickedFaces08, thickness=T7)p.Set(faces=pickedFaces08, name='P08_12_'+str(1+i))注：为了后期边界条件施加的方便，在此次将一系列面定义成一个 Set 。必须通过 append()命令将所有通过循环命令查找的 faces 添加到一个数值中，这样才能将所有的 faces 建立到一个 Set 中去#为中间隔板创建空腔#定义相关参数边界距离、圆角 d0=100r0=100p = mdb.models['Model-1'].parts['Part-1']f1, e1 = p.faces, p.edgest = p.MakeSketchTransform(f.findAt(coordinates=(0, 0.0, 500.0)),sketchUpEdge=e.findAt(coordinates=(W0/2+W1/2, 0.0, 500.0)), sketchPlaneSide=SIDE1, sketchOrientation=RIGHT,origin=(0.0, 0.0, 500.0))s = mdb.models['Model-1'].ConstrainedSketch(name=' profile ', sheetSize=5910.0, gridSpacing=147.0, transform=t)g, v, d1, c = s.geometry, s.vertices, s.dimensions, s.constraintss.setPrimaryObject(option=SUPERIMPOSE)p = mdb.models['Model-1'].parts['Part-1']p.projectReferencesOntoSketch(sketch=s, filter=COPLANAR_EDGES) #创建矩形s.rectangle(point1=(-W0/2-W1/2+d0, H0/2-d0), point2=(W0/2+W1/2-d0, -H0/2+d0)) #创建圆角s.FilletByRadius(radius=r0, curve1=g[29], nearPoint1=(-W0/2-W1/2+d0,H0/2-d0), curve2=g[26], nearPoint2=(-W0/2-W1/2+d0, H0/2-d0)) s.FilletByRadius(radius=r0, curve1=g[26], nearPoint1=(-W0/2-W1/2+d0,-H0/2+d0), curve2=g[27], nearPoint2=(-W0/2-W1/2+d0, -H0/2+d0)) s.FilletByRadius(radius=r0, curve1=g[27], nearPoint1=(W0/2+W1/2-d0,-H0/2+d0), curve2=g[28], nearPoint2=(W0/2+W1/2-d0, -H0/2+d0)) s.FilletByRadius(radius=r0, curve1=g[28], nearPoint1=(W0/2+W1/2-d0,H0/2-d0), curve2=g[29], nearPoint2=(W0/2+W1/2-d0, H0/2-d0)) p = mdb.models['Model-1'].parts['Part-1']f1, d2 = p.faces, p.datums注：圆制圆角进行参的原点最好通p.CutExtrude(f.findAt(coordinates=(0, 0.0, 500.0)),sketchUpEdge=e.findAt(coordinates=(W0/2+W1/2, 0.0, 500.0)), sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, sketch=s, depth=L0, flipExtrudeDirection=OFF)s.unsetPrimaryObject()del mdb.models['Model-1'].sketches[' profile ']注：圆角有方向性，因此在绘制圆角时需要将 nearpoint 也进行参数化，可直接选择草图的原点。另外，此处的 curve最好通过 findAt 查找得出。#开始建立梁Beam_1p = mdb.models['Model-1'].parts['Part-1'] f, d = p.faces, p.datums#绘制参考面 p.DatumPlaneByOffset(plane=f.findAt(coordinates=(W0/2, -H0/2, 100.0)),flip=SIDE2, offset=8.0)dp1 = d.keys()[-1]p = mdb.models['Model-1'].parts['Part-1'] d = p.datumst = p.MakeSketchTransform(sketchPlane=d[dp1], sketchUpEdge=d[4].axis1, sketchPlaneSide=SIDE1, sketchOrientation=RIGHT, origin=(0.0, 0.0,0.0))s = mdb.models['Model-1'].ConstrainedSketch(name=' profile ', sheetSize=31857.0, gridSpacing=796.0, transform=t)g, v, d1, c = s.geometry, s.vertices, s.dimensions, s.constraints s.setPrimaryObject(option=SUPERIMPOSE)p = mdb.models['Model-1'].parts['Part-1']注：此处建立参考面后，立即给该参考面进行了编号(dp1)，否则后面的程序中无法引用该参考面。实际上，每建立一个参考后，都应该给该参考进行编号，这样的操作才比较规范。注：通过参考面的编号[dp1]来引用参考面。#计算中间加强梁的数量if n%2==1:n1=n//2n2=n//2 else:n1=n//2 n2=n//2-1for i in range(0,n1):s.Line(point1=(-500-i*2520*2, W0/2+W1/2), point2=(-500-2520-i*2520*2,-W0/2-W1/2 )) for i in range(0,n2):s.Line(point1=(-500-2520-i*2520*2,-W0/2-W1/2), point2=(-500-2*2520-i*2520*2,W0/2+W1/2 ))#在基准平面 dp1 上面绘制梁p = mdb.models['Model-1'].parts['Part-1'] d2 = p.datumse = p.edgesp.Wire(sketchPlane=d2[dp1], sketchUpEdge=d2[4].axis1, sketchPlaneSide=SIDE1,sketchOrientation=RIGHT, sketch=s)s.unsetPrimaryObject()del mdb.models['Model-1'].sketches[' profile ']edges1=[]for i in range(0,n-1):edges1.append(e.findAt(((0, -H0/2-8, 500+2520/2+i*2520),),))p.Set(edges=edges1, name='Beam_1')注：必须通过 append()命令将所有通过循环命令查找的edges 添加到一个数组中，这样才能将所有的edges 建立到一个 Set 中去，以方便后期建立 tie。############################开始定义有限元分析的相关参数 #定义材料mdb.models['Model-1'].Material(name='steel')mdb.models['Model-1'].materials['steel'].Elastic(table=((210000.0, 0.3), ))mdb.models['Model-1'].materials['steel'].Density(table=((7.8e-06, ), ))#定义壳单元属性mdb.models['Model-1'].HomogeneousShellSection(name='shell', preIntegrate=OFF, material='steel', thicknessType=UNIFORM, thickness=10.0, thicknessField='', idealization=NO_IDEALIZATION, poissonDefinition=DEFAULT, thicknessModulus=None, temperature=GRADIENT, useDensity=OFF, integrationRule=SIMPSON, numIntPts=5)#赋所有壳单元属性p = mdb.models['Model-1'].parts['Part-1']for i in range(1,5): region1 = p.sets['P0'+str(i)+'_12'] p.SectionAssignment(region=region1, sectionName='shell', offset=0.0, offsetType=FROM_GEOMETRY, offsetField='', thicknessAssignment=FROM_GEOMETRY)region2 = p.sets['P05_08']p.SectionAssignment(region=region2, sectionName='shell', offset=0.0,offsetType=FROM_GEOMETRY, offsetField='', thicknessAssignment=FROM_GEOMETRY)for i in range(1,n+1):region3 = p.sets['P06_08_'+str(i)]p.SectionAssignment(region=region3, sectionName='shell', offset=0.0,offsetType=FROM_GEOMETRY, offsetField='', thicknessAssignment=FROM_GEOMETRY)for i in range(1,n+1):region4 = p.sets['P07_12_'+str(i)]p.SectionAssignment(region=region4, sectionName='shell', offset=0.0,offsetType=FROM_GEOMETRY, offsetField='', thicknessAssignment=FROM_GEOMETRY)for i in range(1,n+1):region5 = p.sets['P08_12_'+str(i)]p.SectionAssignment(region=region5, sectionName='shell', offset=0.0,offsetType=FROM_GEOMETRY, offsetField='',thicknessAssignment=FROM_GEOMETRY)注：此处选择厚度属性来源于几何。如果需要做厚度优化的话，也可以选择来源于壳单元属性，但需要建立与之匹配的壳单元属性，并且一个零件对应于一个壳单元熟悉。注：全部通过前期建立的Set来赋壳单元属性，省掉了再次findAt 的麻烦。#定义梁单元属性mdb.models['Model-1'].LProfile(name='L_65', a=65.0, b=65.0, t1=7.0, t2=7.0) mdb.models['Model-1'].BeamSection(name='B_65', integration=DURING_ANALYSIS,poissonRatio=0.0, profile='L_65', material='steel', temperatureVar=LINEAR, consistentMassMatrix=False)#赋所有梁单元属性p = mdb.models['Model-1'].parts['Part-1'] region = p.sets['Beam_1']p.SectionAssignment(region=region, sectionName='B_65', offset=0.0,offsetType=MIDDLE_SURFACE, offsetField='', thicknessAssignment=FROM_SECTION)p.assignBeamSectionOrientation(region=region, method=N1_COSINES, n1=(0.0, 0.0,-1.0))#定义装配体 import assemblya = mdb.models['Model-1'].rootAssembly a.DatumCsysByDefault(CARTESIAN)p = mdb.models['Model-1'].parts['Part-1']a.Instance(name='Part-1-1', part=p, dependent=ON)#定义分析步 import stepmdb.models['Model-1'].StaticStep(name='Step-1', previous='Initial')#定义底面与梁的tiedimport interactiona = mdb.models['Model-1'].rootAssembly region1=a.instances['Part-1-1'].sets['P04_12'] region2=a.instances['Part-1-1'].sets['Beam_1']mdb.models['Model-1'].Tie(name='Constraint-1', master=region1, slave=region2,positionToleranceMethod=COMPUTED, adjust=OFF, tieRotations=ON, thickness=ON)#开始定义耦合#导入相关模块 import regionToolseta = mdb.models['Model-1'].rootAssemblyd, r = a.datums, a.referencePoints#定义参考点a.ReferencePoint(point=(0.0, H0/2, 500+2520/2)) r1 = a.referencePointsrp1 = r.keys()[-1]refPoints1=(r1[rp1], ) region1=regionToolset.Region(referencePoints=refPoints1) s1 = a.instances['Part-1-1'].facesregion2 = a.instances['Part-1-1'].sets['P07_fp']mdb.models['Model-1'].Coupling(name='Constraint-2', controlPoint=region1, surface=region2, influenceRadius=WHOLE_SURFACE, couplingType=DISTRIBUTING,localCsys=None, u1=ON, u2=ON, u3=ON, ur1=ON, ur2=ON, ur3=ON)注：对建立的参考点编号，以方便后期调用。#########################定义边界条件 import loada = mdb.models['Model-1'].rootAssembly d, r = a.datums, a.referencePointsregion = a.instances['Part-1-1'].sets['P02_12']mdb.models['Model-1'].DisplacementBC(name='SPC', createStepName='Initial', region=region, u1=SET, u2=SET, u3=SET, ur1=SET, ur2=SET, ur3=SET, amplitude=UNSET, distributionType=UNIFORM, fieldName='', localCsys=None)a = mdb.models['Model-1'].rootAssemblyregion = a.instances['Part-1-1'].sets['P08_12_'+str(n-1)]mdb.models['Model-1'].DisplacementBC(name='SPC2', createStepName='Initial', region=region, u1=SET, u2=SET, u3=SET, ur1=SET, ur2=SET, ur3=SET, amplitude=UNSET, distributionType=UNIFORM, fieldName='', localCsys=None)r1 = a.referencePoints refPoints1=(r1[rp1], )region = regionToolset.Region(referencePoints=refPoints1)mdb.models['Model-1'].ConcentratedForce(name='force', createStepName='Step-1',region=region, cf2=-10000.0, distributionType=UNIFORM, field='',localCsys=None)mdb.models['Model-1'].Gravity(name='G', createStepName='Step-1', comp2=-9.8,distributionType=UNIFORM, field='')#################划分网格 import meshp = mdb.models['Model-1'].parts['Part-1'] p.seedPart(size=20.0, deviationFactor=0.1, minSizeFactor=0.1) p.generateMesh()a = mdb.models['Model-1'].rootAssembly###############创建作业并提交分析 import jobmdb.Job(name='006', model='Model-1', description='', type=ANALYSIS, atTime=None, waitMinutes=0, waitHours=0, queue=None, memory=90, memoryUnits=PERCENTAGE, getMemoryFromAnalysis=True, explicitPrecision=SINGLE, nodalOutputPrecision=SINGLE, echoPrint=OFF, modelPrint=OFF, contactPrint=OFF, historyPrint=OFF, userSubroutine='', scratch='', multiprocessingMode=DEFAULT, numCpus=4, numDomains=4)mdb.jobs['006'].submit(consistencyChecking=ON) mdb.jobs['006'].waitForCompletion()###############进入后处理模块 import visualizationo3 = session.openOdb(name='F:/ABAQUS/006.odb') session.viewports['Viewport: 1'].setValues(displayedObject=o3) session.viewports['Viewport: 1'].odbDisplay.display.setValues(plotState=(CONTOURS_ON_DEF, ))session.viewports['Viewport: 1'].view.setValues(session.views['Iso'])mdb.saveAs(pathName='F:/ABAQUS/006.cae')来源：CAE仿真学社
