Ansys APDL (經(jīng)典)完整框架分析—Ansys經(jīng)典培訓(xùn)

2017-03-18  by:CAE仿真在線  來源:互聯(lián)網(wǎng)

Ansys經(jīng)典培訓(xùn) 選仿真在線

這是一個Ansys APDL (經(jīng)典)完整分析框架,還在學(xué)習(xí)如何寫apdl代碼的同學(xué),可以參考:

!********************提示********************************************
!第一步:建立框架結(jié)構(gòu)模型
!第二步:框架結(jié)構(gòu)施加重力荷載
!第三步:框架結(jié)構(gòu)施加活荷載
!第四步:框架結(jié)構(gòu)施加風(fēng)荷載
!第五步:框架結(jié)構(gòu)荷載組合運(yùn)算
!第六步:框架結(jié)構(gòu)模態(tài)分析
!第七步:框架結(jié)構(gòu)屈曲特征值分析
!第八步:框架結(jié)構(gòu)地震時程彈性分析
!第九步:結(jié)束

!采用地震波時間文件為:TIME.TXT
!采用地震波文件分別為:AC_X.TXT/AC_Y.TXT

FINISH
/CLEAR
/FILENAME,FRAME_SHEAR_WALL
/TITLE, FRAME_SHEAR_WALL

!**************************************************************************
!************************第一步********************************************
!********************框架結(jié)構(gòu)建模型***************************************

/PREP7

!采用單位為N/m/S國際單位制

!定義單元類型
ET,1,BEAM4
ET,2,SHELL63

!定義實常數(shù)
R,1,0.25,0.0052,0.0052,0.5,0.5
R,2,0.2025,0.0034,0.0034,0.45,0.45
R,3,0.06,0.0002,0.00045,0.3,0.2
R,4,0.25,0.25,0.25,0.25
R,5,0.1,0.1,0.1,0.1

!定義材料參數(shù)
MP,EX,1,3.0E10
MP,NUXY,1,0.2
MP,DENS,1,2500

!關(guān)鍵點
*DO,II,1,1
K,1+(II-1)*20,0,0,(II-1)*6
K,2+(II-1)*20,6,0,(II-1)*6
K,3+(II-1)*20,12,0,(II-1)*6
K,4+(II-1)*20,17,0,(II-1)*6
K,5+(II-1)*20,0,5,(II-1)*6
K,6+(II-1)*20,6,5,(II-1)*6
K,7+(II-1)*20,12,5,(II-1)*6
K,8+(II-1)*20,17,5,(II-1)*6
K,9+(II-1)*20,0,10,(II-1)*6
K,10+(II-1)*20,6,10,(II-1)*6
K,11+(II-1)*20,12,10,(II-1)*6
K,12+(II-1)*20,17,10,(II-1)*6
K,14+(II-1)*20,6,1.875,(II-1)*6
K,16+(II-1)*20,6,3.125,(II-1)*6
K,18+(II-1)*20,6,1.875,3.9
K,20+(II-1)*20,6,3.125,3.9
*ENDDO

*DO,II,1,10
K,1+II*20,0,0,(II-1)*3+6
K,2+II*20,6,0,(II-1)*3+6
K,3+II*20,12,0,(II-1)*3+6
K,4+II*20,17,0,(II-1)*3+6
K,5+II*20,0,5,(II-1)*3+6
K,6+II*20,6,5,(II-1)*3+6
K,7+II*20,12,5,(II-1)*3+6
K,8+II*20,17,5,(II-1)*3+6
K,9+II*20,0,10,(II-1)*3+6
K,10+II*20,6,10,(II-1)*3+6
K,11+II*20,12,10,(II-1)*3+6
K,12+II*20,17,10,(II-1)*3+6
K,13+II*20,0,1.875,(II-1)*3+6
K,14+II*20,6,1.875,(II-1)*3+6
K,15+II*20,0,3.125,(II-1)*3+6
K,16+II*20,6,3.125,(II-1)*3+6
K,17+II*20,0,1.875,(II-1)*3+6+1.5
K,18+II*20,6,1.875,(II-1)*3+6+2
K,19+II*20,0,3.125,(II-1)*3+6+1.5
K,20+II*20,6,3.125,(II-1)*3+6+2
*ENDDO

*DO,II,11,11
K,1+II*20,0,0,(II-1)*3+6
K,2+II*20,6,0,(II-1)*3+6
K,3+II*20,12,0,(II-1)*3+6
K,4+II*20,17,0,(II-1)*3+6
K,5+II*20,0,5,(II-1)*3+6
K,6+II*20,6,5,(II-1)*3+6
K,7+II*20,12,5,(II-1)*3+6
K,8+II*20,17,5,(II-1)*3+6
K,9+II*20,0,10,(II-1)*3+6
K,10+II*20,6,10,(II-1)*3+6
K,11+II*20,12,10,(II-1)*3+6
K,12+II*20,17,10,(II-1)*3+6
K,13+II*20,0,1.875,(II-1)*3+6
K,14+II*20,6,1.875,(II-1)*3+6
K,15+II*20,0,3.125,(II-1)*3+6
K,16+II*20,6,3.125,(II-1)*3+6
K,17+II*20,0,1.875,(II-1)*3+6+1.8
K,18+II*20,6,1.875,(II-1)*3+6+2.5
K,19+II*20,0,3.125,(II-1)*3+6+1.8
K,20+II*20,6,3.125,(II-1)*3+6+2.5
*ENDDO

*DO,II,12,12
K,1+II*20,0,0,39.5
K,2+II*20,6,0,39.5
K,3+II*20,12,0,39.5
K,4+II*20,17,0,39.5
K,5+II*20,0,5,39.5
K,6+II*20,6,5,39.5
K,7+II*20,12,5,39.5
K,8+II*20,17,5,39.5
K,9+II*20,0,10,39.5
K,10+II*20,6,10,39.5
K,11+II*20,12,10,39.5
K,12+II*20,17,10,39.5
*ENDDO

*DO,II,2,13
L,(II-1)*20+1,(II-1)*20+2
L,(II-1)*20+2,(II-1)*20+3
L,(II-1)*20+3,(II-1)*20+4
L,(II-1)*20+5,(II-1)*20+6
L,(II-1)*20+6,(II-1)*20+7
L,(II-1)*20+7,(II-1)*20+8
L,(II-1)*20+9,(II-1)*20+10
L,(II-1)*20+10,(II-1)*20+11
L,(II-1)*20+11,(II-1)*20+12
L,(II-1)*20+5,(II-1)*20+9
L,(II-1)*20+6,(II-1)*20+10
L,(II-1)*20+3,(II-1)*20+7
L,(II-1)*20+7,(II-1)*20+11
L,(II-1)*20+4,(II-1)*20+8
L,(II-1)*20+8,(II-1)*20+12
*ENDDO

*DO,II,1,12
L,(II-1)*20+1,II*20+1
L,(II-1)*20+2,II*20+2
L,(II-1)*20+3,II*20+3
L,(II-1)*20+4,II*20+4
L,(II-1)*20+5,II*20+5
L,(II-1)*20+6,II*20+6
L,(II-1)*20+7,II*20+7
L,(II-1)*20+8,II*20+8
L,(II-1)*20+9,II*20+9
L,(II-1)*20+10,II*20+10
L,(II-1)*20+11,II*20+11
L,(II-1)*20+12,II*20+12
*ENDDO


*DO,II,1,1
L,(II-1)*20+14,(II-1)*20+18
L,(II-1)*20+16,(II-1)*20+20
*ENDDO

*DO,II,2,12
L,(II-1)*20+13,(II-1)*20+17
L,(II-1)*20+15,(II-1)*20+19
L,(II-1)*20+14,(II-1)*20+18
L,(II-1)*20+16,(II-1)*20+20
*ENDDO

A, 1, 21, 25, 5

*DO,II,2,12
A, (II-1)*20+1, II*20+1, II*20+5, (II-1)*20+5, (II-1)*20+15, (II-1)*20+19, (II-1)*20+17, (II-1)*20+13
*ENDDO

*DO,II,1,12
A, (II-1)*20+2, II*20+2, II*20+6, (II-1)*20+6, (II-1)*20+16, (II-1)*20+20, (II-1)*20+18, (II-1)*20+14
*ENDDO

*DO,II,1,12
A, II*20+1, II*20+2, II*20+6, II*20+5
A, II*20+2, II*20+3, II*20+7, II*20+6
A, II*20+3, II*20+4, II*20+8, II*20+7
A, II*20+5, II*20+6, II*20+10,II*20+9
A, II*20+6, II*20+7, II*20+11,II*20+10
A, II*20+7, II*20+8, II*20+12,II*20+11
*ENDDO

!立柱網(wǎng)格劃分
LSEL,S,,,181,192!底層立柱
LATT,1,1,1
LESIZE,ALL,,,10
LMESH,ALL

LSEL,S,,,192,324!2~12層立柱
LATT,1,2,1
LESIZE,ALL,,,5
LMESH,ALL

!梁網(wǎng)格劃分
LSEL,S,,,1,180
LATT,1,3,1,
LESIZE,ALL,,,8
LMESH,ALL

!剪力墻網(wǎng)格劃分
LSEL,S,,,372!外剪力墻兩端、內(nèi)剪力墻頂端
LSEL,A,,,413
LSEL,A,,,461
LESIZE,ALL,,,8

LSEL,s,,,418!內(nèi)剪力墻底端
LSEL,A,,,420
LESIZE,ALL,,,3

LSEL,s,,,325!內(nèi)剪力墻底端內(nèi)側(cè)
LSEL,A,,,326
LESIZE,ALL,,,6

LSEL,S,,,375!剪力墻空洞頂部
LSEL,A,,,379
LSEL,A,,,383
LSEL,A,,,387
LSEL,A,,,391
LSEL,A,,,395
LSEL,A,,,399
LSEL,A,,,403
LSEL,A,,,407
LSEL,A,,,411
LSEL,A,,,415
LSEL,A,,,419
LSEL,A,,,423
LSEL,A,,,427
LSEL,A,,,431
LSEL,A,,,435
LSEL,A,,,439
LSEL,A,,,443
LSEL,A,,,447
LSEL,A,,,451
LSEL,A,,,455
LSEL,A,,,459
LSEL,A,,,463
LESIZE,ALL,,,2

!剪力墻網(wǎng)格劃分
ASEL,S,,,1,24
AATT,1,4,2
AMESH,ALL

!樓板網(wǎng)格劃分
ASEL,S,,,25,96
AATT,1,5,2
AMESH,ALL


NSEL,S,LOC,Z,0!選取模型底端節(jié)點
D,ALL,ALL!施加位移約束
ALLSEL,ALL!重新選取所有節(jié)點

/eshape,1.0

/VIEW,1,1,1,1
/ANG,1,270,XM,0
/REPlot


FINISH


!**************************************************************************
!************************第二步********************************************
!********************框架結(jié)構(gòu)施加重力荷載*********************************
!框架結(jié)構(gòu)施加重力荷載
FINISH
/SOLU
ANTYPE,STATIC
NSEL,S,LOC,Z,0!選取模型底端節(jié)點
D,ALL,ALL!施加位移約束
ALLSEL,ALL!重新選取所有節(jié)點
ACEL,0,0,9.8
SOLVE
FINISH


/POST1
SET,FIRST
PLNSOL,U,Z,0,1
FINISH

!Ansys經(jīng)典培訓(xùn) 選仿真在線

!**************************************************************************
!************************第三步********************************************
!*************框架結(jié)構(gòu)施加樓面活荷載D=3KN/M^2*****************************
!框架結(jié)構(gòu)施加樓面活荷載D=3KN/M^2
FINISH
/SOLU
ANTYPE,STATIC
NSEL,S,LOC,Z,0!選取模型底端節(jié)點
D,ALL,ALL!施加位移約束
ALLSEL,ALL!重新選取所有節(jié)點
ACEL,0,0,9.8
SOLVE
FINISH


/POST1
SET,FIRST
PLNSOL,U,Z,0,1
FINISH


!**************************************************************************
!************************第四步********************************************
!***********框架結(jié)構(gòu)施加風(fēng)荷載(基本風(fēng)壓=0.25KN/M^2,體形系數(shù)為1.0**********
!框架結(jié)構(gòu)施加風(fēng)荷載(先Y方向,后X方向)分兩次分別施加
FINISH
/SOLU
ANTYPE,STATIC
*DIM,LOAD_1,ARRAY,12
LOAD_1(1)=3.78,2.16,2.39,2.57,2.72,2.84,2.95,3.17,3.20,3.29,3.39,3.51

*DIM,LOAD_2,ARRAY,12
LOAD_2(1)=7.56,4.32,4.78,5.14,5.44,5.68,5.90,6.34,6.40,6.58,6.76,7.02

*DIM,LOAD_3,ARRAY,12
LOAD_3(1)=6.93,3.96,4.38,4.71,4.99,5.21,5.41,5.81,5.87,6.03,6.20,6.44

*DIM,LOAD_4,ARRAY,12
LOAD_4(1)=3.15,1.80,1.99,2.14,2.27,2.37,2.46,2.64,2.67,2.74,2.82,2.93


*DIM,LOAD_A,ARRAY,12
LOAD_A(1)=3.15,1.80,1.99,2.14,2.27,2.37,2.46,2.64,2.67,2.74,2.82,2.93

*DIM,LOAD_B,ARRAY,12
LOAD_B(1)=6.30,3.60,3.98,4.28,4.54,4.74,4.92,5.28,5.34,5.48,5.64,5.86

*DIM,LOAD_C,ARRAY,12
LOAD_C(1)=3.15,1.80,1.99,2.14,2.27,2.37,2.46,2.64,2.67,2.74,2.82,2.93

*DO,II,1,12
FK,1+20*II,FY,LOAD_1(II)
*ENDDO

*DO,II,1,12
FK,2+20*II,FY,LOAD_2(II)
*ENDDO

*DO,II,1,12
FK,3+20*II,FY,LOAD_3(II)
*ENDDO

*DO,II,1,12
FK,4+20*II,FY,LOAD_4(II)
*ENDDO

SOLVE


FKDELE,ALL,ALL!第二次施加風(fēng)荷載,刪除第一次的。風(fēng)有方向性
*DO,II,1,12
FK,1+20*II,FX,LOAD_A(II)
*ENDDO

*DO,II,1,12
FK,5+20*II,FX,LOAD_B(II)
*ENDDO

*DO,II,1,12
FK,9+20*II,FX,LOAD_C(II)
*ENDDO

SOLVE
FINISH

/POST1
SET,FIRST
PLNSOL,U,Y,0,1
SET,NEXT,
PLNSOL,U,X,0,1
FINISH

!**************************************************************************
!************************第五步********************************************
!************************框架結(jié)構(gòu)荷載組合計算********************************
!框架結(jié)構(gòu)荷載組合計算(1.D+L+WIND_X;2.D+L+WIND_Y)


!**************************************************************************
!************************第六步********************************************
!*******************框架結(jié)構(gòu)模態(tài)分析**************************************
!框架結(jié)構(gòu)模態(tài)分析
FINISH
/SOLU
ANTYPE,MODAL
MODOPT,LANB,6
MODOPT,LANB,6,0,0,,OFF
SOLVE
FINISH

/POST1
SET,LIST
SET,FIRST
PLDISP,0
SET,NEXT
PLSISP,0
SET,NEXT
PLSISP,0
SET,NEXT
PLSISP,0
SET,NEXT
PLSISP,0
SET,NEXT
PLSISP,0

FINISH

!**************************************************************************
!************************第七步********************************************
!****************框架結(jié)構(gòu)特征值屈曲分析***********************************
!框架結(jié)構(gòu)特征值屈曲分析
FINISH
/SOLU
ANTYPE,0
EQSLV,SPAR
PSTRES,ON
SOLVE
FINISH


/SOLU
ANTYPE,1
BUCOPT,LANB,6,0,0
MXPAND,6,0,0,1,0.001,
SOLVE
FINISH


/POST1
SET,LIST
SET,FIRST
PLDISP,2
SET,NEXT
PLDISP,2
SET,NEXT
PLDISP,2
SET,NEXT
PLDISP,2
SET,NEXT
PLDISP,2
SET,NEXT
PLDISP,2

FINISH


!**************************************************************************
!************************第八步********************************************
!****************框架結(jié)構(gòu)地震時程分析*************************************
!框架結(jié)構(gòu)地震時程分析
FINISH
*SET,NT,150
*DIM,TIME,,NT
*DIM,AC_X,,NT
*DIM,AC_Y,,NT

*CREATE,time
*VREAD,TIME,'TIME','txt',' ',1, , , , , ,
(F6.2)
*END
/INPUT,time

*CREATE,ac_x
*VREAD,AC_X,'AC_X','txt',' ',1, , , , , ,
(E10.3)
*END
/INPUT,ac_x

*CREATE,ac_y
*VREAD,AC_Y,'AC_Y','txt',' ',1, , , , , ,
(E10.3)
*END
/INPUT,ac_y

!Ansys經(jīng)典培訓(xùn) 選仿真在線
!分析選項設(shè)置與求解
/SOLU!進(jìn)入求解器
ANTYPE,TRANS!定義分析類型
NSUBST,1, , ,1!定義荷載子步數(shù)
*DO,II,1,NT
!施加加速度荷載
ACEL,AC_X(II),AC_Y(II)
TIME,TIME(II)!設(shè)置時間點
SOLVE!求解
*ENDDO

FINISH

/POST26
NSOL,2,733,U,X,UX_1
NSOL,3,773,U,X,UX_2
NSOL,4,748,U,X,UX_3
NSOL,5,788,U,X,UX_4

NSOL,6,733,U,Y,UY_1
NSOL,7,773,U,Y,UY_2
NSOL,8,748,U,Y,UY_3
NSOL,9,788,U,Y,UY_4

PLVAR,2,3,4,5
PLVAR,6,7,8,9


FINISH


!**************************************************************************
!************************第九步********************************************
!****************整個框架結(jié)構(gòu)所有分析過程結(jié)束*****************************
FINISH

轉(zhuǎn)自博客:http://blog.sina.com.cn/s/blog_713bace90100w691.html


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