en:example:plas:11:1
Table of Contents
Quadrilaterals, BEAM6P10
Problem
Mesh
| element | type | nodes |
|---|---|---|
| 1 | 6 | 1 3 4 2 12 14 13 11 |
| 2 | 6 | 3 5 6 4 15 17 16 14 |
| 3 | 6 | 5 7 8 6 18 20 19 17 |
| 4 | 6 | 7 9 10 8 21 23 22 20 |
Boundary conditions
$u=v=0$ at node 1
$v=0$ at nodes 3, 5, 7, 9, 12, 15, 18, 21
Computation
The computation is executed with the following commands:
- beam6p10.bat
rmd2 beam6p10.i1 rpd2 beam6p10.i2 srh2 beam6p10.i3 fefs beam6p10.i4 hpp2 beam6p10.iP hpls beam6p10.iL str2 beam6p10.i5
Input
- beam6p10.i1
; NELEM NNOD ITED ... KSS IP 4 23 6 6*0 -1 ; CRIT SCALE THDEF RP 1.01 1 0.01 XY N 1:10 X 2*0 2*0.25 2*0.5 2*0.75 2*1 Y 5*(0 0.02) EL E 1:4 N =A 1 3 4 2 =A =B 12 14 13 11 =B =2A =3B =4A =6B =6A =9B EN EN
- beam6p10.i2
; KREST IP 1 ; E α ν ρ MP 1 T 1 V 2.1e11 0 0.3 7850 4*0 ; k0 κ1 κ2 a1 a2 c0 150e6 10e9 8e-9 50e9 10e-9 8e-9 NV 1 T 3 N 2 V 0 1e15 0 NV 2 T 3 N 4 V 0 1e15 0 NV 3 T 3 N 6 V 0 1e15 0 NV 4 T 3 N 8 V 0 1e15 0 NV 5 T 3 N 10 V 0 1e15 0 NV 6 T 3 N 13 V 0 1e15 0 NV 7 T 3 N 16 V 0 1e15 0 NV 8 T 3 N 19 V 0 1e15 0 NV 9 T 3 N 22 V 0 1e15 0 NV 10 T 6 V 0 100e9 0 0 0 NV 11 T 6 V 0 -40e9 0 0 0 NV 12 T 6 V 0 90e9 0 0 0 SV 1 T 9 V 150e6 0 0 SV 2 T 9 V -150e6 0 0 SV 3 T 9 V 0 150e6 0 SV 4 T 9 V 0 -150e6 0 AS 1 /M 1 /B0 C 1 2 N 1 /B0 C 2 N 3 5 7 9 12 15 18 21 /N 1 E 1 /N 2 E 2 /N 3 E 3 /N 4 E 4 /N 5 E 4 /N 6 E 1 /N 7 E 2 /N 8 E 3 /N 9 E 4 AS 2 /N 10 N 2 4 6 8 10 13 16 19 22 AS 3 /N 11 N 2 4 6 8 10 13 16 19 22 AS 4 /N 12 N 2 4 6 8 10 13 16 19 22 AS 5 /N 12 N 2 4 6 8 10 13 16 19 22 /S 1 E 1:4 S3 /S 2 E 1:4 S1 /S 3 E 4 S2 /S 4 E 1 S4 AS 6 /N 12 N 2 4 6 8 10 13 16 19 22 /S 1 E 1:4 S1 /S 2 E 1:4 S3 /S 3 E 1 S4 /S 4 E 4 S2 EN EN
- beam6p10.i3
; KREST IP 1 EN EN
- beam6p10.i4
; KREST IP 1 EN EN
- beam6p10.iP
; KREST NLC NCYC KMOD ... IP 1 11 0 4 6*0 ; load case sequence 2 3 2 3 2 4 5 6 5 6 5 EN EN
- beam6p10.iL
; KMET KOUT NSUBI NITER NINT KTPR IP 0 1 0 1000 100 0 ; UTOL RTOL XTOL PENAL RP 1e-8 1e-8 0 0 EN EN
- beam6p10.i5
; KLC 0 KOUT ILC ... KPROB KGRAF IP 3 0 1 11 6*0 2 2 EN EN
Output
- beam6p10.o5
; KLC 0 KOUT ILC ... KPROB KGRAF IP 3 0 1 11 6*0 2 2 EN EN PLANE STRESS 1TH LOAD CASE DISPLACEMENTS NODE U V [m] [m] 1 0.0000000E+00 0.0000000E+00 2 0.8934028E-04 0.9000000E-04 3 -0.5608892E-03 0.0000000E+00 4 -0.4715489E-03 0.9000000E-04 5 -0.1121778E-02 0.0000000E+00 6 -0.1032438E-02 0.9000000E-04 7 -0.1682667E-02 0.0000000E+00 8 -0.1593327E-02 0.9000000E-04 9 -0.2243557E-02 0.0000000E+00 10 -0.2154216E-02 0.9000000E-04 11 0.4467014E-04 0.4500000E-04 12 -0.2804446E-03 0.0000000E+00 13 -0.1911043E-03 0.8999999E-04 14 -0.5162190E-03 0.4500000E-04 15 -0.8413337E-03 0.0000000E+00 16 -0.7519935E-03 0.8999999E-04 17 -0.1077108E-02 0.4500000E-04 18 -0.1402223E-02 0.0000000E+00 19 -0.1312883E-02 0.8999999E-04 20 -0.1637997E-02 0.4500000E-04 21 -0.1963112E-02 0.0000000E+00 22 -0.1873772E-02 0.8999999E-04 23 -0.2198887E-02 0.4500000E-04 STRESSES AT GAUSS POINTS IE IGP XG YG SIG-X SIG-Y SIG-XY SIG-Z HMH EPSP DMG [m] [m] [MPa] [MPa] [MPa] [MPa] [MPa] [-] [%] 1 1 0.28175E-01 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 2 0.12500E+00 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 3 0.22182E+00 0.22540E-02 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 4 0.28175E-01 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 5 0.12500E+00 0.10000E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 6 0.22182E+00 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 7 0.28175E-01 0.17746E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 8 0.12500E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 9 0.22182E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 2 1 0.27818E+00 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 2 0.37500E+00 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 3 0.47182E+00 0.22540E-02 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 4 0.27818E+00 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 5 0.37500E+00 0.10000E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 6 0.47182E+00 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 7 0.27818E+00 0.17746E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 8 0.37500E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 9 0.47182E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 3 1 0.52818E+00 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 2 0.62500E+00 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 3 0.72182E+00 0.22540E-02 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 4 0.52818E+00 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 5 0.62500E+00 0.10000E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 6 0.72182E+00 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 7 0.52818E+00 0.17746E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 8 0.62500E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 9 0.72182E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 4 1 0.77818E+00 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 2 0.87500E+00 0.22540E-02 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 3 0.97182E+00 0.22540E-02 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 4 0.77818E+00 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 5 0.87500E+00 0.10000E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 6 0.97182E+00 0.10000E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 7 0.77818E+00 0.17746E-01 -0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 8 0.87500E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 9 0.97182E+00 0.17746E-01 0.0 4.9 150.0 -0.1 259.9 0.2904E-01 0.00 * END OF STR3 * TOTAL CPU: 00:00:00
en/example/plas/11/1.txt · Last modified: 2024-11-07 09:48 by Petr Pařík