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CommandListHW1 - modify.txt
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CommandListHW1 - modify.txt
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!**********************
!PROBLEM: HOMEWORK 1 *
!**********************
FINISH
/CLEAR, START, NEW
/TITLE, HOMERWORK 1
/EFACET,4
/GFILE,2400
/PLOPTS,DATE,0
! >>>>> PARAMETRI MODELLO <<<<<
*SET, bottom_chord, 4000
*SET, top_chord, 4000
*SET, h_struts, 4000
*SET, o_struts, 3500
*SET, ndiv, 16 !numero divisioni
*SET, sez_one, 1000 !sezione bottom_chord,top_chord,struts (mm^2)
*SET, sez_two, 600 !sezione sway_bracing (mm^2)
*SET, sez_three, 400 !sezione lateral_bracing (mm^2)
! >>>>> PROPRIETÀ’ DEL MATERIALE <<<<<
*SET,E_Young, 210000 ! modulo di Young , MPa
*SET,ni,0.3 ! coefficiente di Poisson
! >>>>> CONDIZIONI DI CARICO <<<<<
*SET,F, (20000*(bottom_chord/1000)*6)/7 !carico distribuito, N/mm
/PREP7
ET,1,180
ET,2,180
ET,3,180
R,1,sez_one
R,2,sez_two
R,3,sez_three
MP,EX,1,E_Young
MP,PRXY,1,ni
N,1,0,0,0
N,2,bottom_chord,0,0
N,3,bottom_chord*2,0,0
N,4,bottom_chord*3,0,0
N,5,bottom_chord*4,0,0
N,6,bottom_chord*5,0,0
N,7,bottom_chord*6,0,0
N,8,bottom_chord,h_struts,0
N,9,bottom_chord*2,7700,0
N,10,bottom_chord*3,8000,0
N,11,bottom_chord*4,7700,0
N,12,bottom_chord*5,h_struts,0
N,13,0,0,o_struts
N,14,bottom_chord,0,o_struts
N,15,bottom_chord*2,0,o_struts
N,16,bottom_chord*3,0,o_struts
N,17,bottom_chord*4,0,o_struts
N,18,bottom_chord*5,0,o_struts
N,19,bottom_chord*6,0,o_struts
N,20,bottom_chord,h_struts,o_struts
N,21,bottom_chord*2,7700,o_struts
N,22,bottom_chord*3,8000,o_struts
N,23,bottom_chord*4,7700,o_struts
N,24,bottom_chord*5,h_struts,o_struts
SAVE
!>>>> ELEMENT <<<<
TYPE, 1
Real, 1
Mat, 1
E,1,2
E,2,3
E,3,4
E,4,5
E,5,6
E,6,7
E,8,9
E,9,10
E,10,11
E,11,12
E,13,14
E,14,15
E,15,16
E,16,17
E,17,18
E,18,19
E,20,21
E,21,22
E,22,23
E,23,24
E,1,13
E,2,14
E,3,15
E,4,16
E,5,17
E,6,18
E,7,19
E,1,8
E,12,7
E,24,19
E,13,20
E,2,8
E,3,9
E,4,10
E,5,11
E,6,12
E,14,20
E,15,21
E,16,22
E,17,23
E,18,24
E,8,20
E,9,21
E,10,22
E,11,23
E,12,24
TYPE, 2
Real, 2
Mat, 1
E,8,21
E,9,22
E,10,23
E,11,24
E,20,9
E,21,10
E,22,11
E,23,12
TYPE, 3
Real, 2
Mat, 1
E,3,8
E,4,9
E,4,11
E,5,12
E,20,15
E,21,16
E,16,23
E,17,24
SAVE
!>>>> CONSTRAINT <<<<
D,1,ux,0
D,1,uy,0
D,7,uy,0
D,13,ux,0
D,13,uy,0
D,19,uy,0
D,all,uz,0
!>>>> FORZE <<<<
F,1,fy, -F
F,2,fy, -F
F,3,fy, -F
F,4,fy, -F
F,5,fy, -F
F,6,fy, -F
F,7,fy, -F
F,13,fy, -F
F,14,fy, -F
F,15,fy, -F
F,16,fy, -F
F,17,fy, -F
F,18,fy, -F
F,19,fy, -F
SAVE
!>>>> SOLUTION <<<<
/SOLU
NLGEOM,ON
SOLCONTROL,ON
TIME,1
PIVCHECK,OFF
SOLVE
!>>>> POST-PROCESS <<<<
/POST1
PLDISP,1
PRNSOL,U,COMP
/RGB,INDEX,100,100,100, 0
/RGB,INDEX, 80, 80, 80,13
/RGB,INDEX, 60, 60, 60,14
/RGB,INDEX, 0, 0, 0,15
/REPLOT
/IMAGE, SAVE, Displacement-modify, bmp
/RGB,INDEX, 0, 0, 0, 0
/RGB,INDEX, 60, 60, 60,13
/RGB,INDEX, 80, 80, 80,14
/RGB,INDEX,100,100,100,15
ETABLE,AXIALFORCE,SMISC,1
ETABLE,AXIALSTRESS,LS,1
PLETAB,AXIALFORCE
PLETAB,AXIALSTRESS
PRETAB,AXIALFORCE,AXIALSTRESS
PRRSOL,F