Uchanganuzi wa mwitikio wa masafa¶
Uchanganuzi huu unatumia data katika tutorial/17_freq_beam.
Kitu cha uchanganuzi¶
Kitu cha uchanganuzi ni cantilever beam; umbo linaonyeshwa katika Mchoro 4.17.1 na data ya mesh katika Mchoro 4.17.2.
| Kipengee | Maelezo | Dokezo | Rejea |
|---|---|---|---|
| Aina ya uchanganuzi | Uchanganuzi wa mwitikio wa masafa | !SOLUTION,TYPE=EIGEN !SOLUTION,TYPE=DYNAMIC | |
| Idadi ya nodi | 55 | ||
| Idadi ya vipengele | 126 | ||
| Aina ya kipengele | Tetrahedron ya nodi 4, daraja la kwanza | !ELEMENT,TYPE=341 | |
| Jina la sifa ya nyenzo | Material-1 | !MATERIAL,NAME=Material-1 | |
| Masharti ya mpaka | Kizuizi, concentrated load, eigenvalue | !EIGENREAD | |
| Mbinu ya solver ya matriki | CG/SSOR | !SOLVER,METHOD=CG,PRECOND=1 |
Maudhui ya uchanganuzi¶
Tunafanya uchanganuzi wa mwitikio wa masafa kwa kufunga kabisa mwisho mmoja wa cantilever beam na kutumia concentrated load kwenye nodi mbili za mwisho wa upande mwingine.
Kwanza tunafanya modal analysis hadi mode ya 10 kwa masharti yale yale ya mpaka, kisha uchanganuzi unafanywa kwa kutumia eigenvalues na eigenvectors hadi mode ya 5. Data ya udhibiti wa uchanganuzi wa mwitikio wa masafa imeonyeshwa hapa chini.
Data ya udhibiti wa uchanganuzi beam_eigen.cnt¶
# Control File for FISTR
!VERSION
3
!WRITE,RESULT
!WRITE,VISUAL
!SOLUTION, TYPE=EIGEN
!EIGEN
10, 1.0E-8, 60
!BOUNDARY
_PickedSet4, 1, 3, 0.0
!SOLVER,METHOD=CG,PRECOND=1,ITERLOG=NO,TIMELOG=YES
10000, 1
1.0e-8, 1.0, 0.0
!VISUAL,method=PSR
!surface_num=1
!surface 1
!output_type=VTK
!END
Data ya udhibiti wa uchanganuzi beam_freq.cnt¶
# Control File for FISTR
!VERSION
3
!WRITE,RESULT
!WRITE,VISUAL
!SOLUTION, TYPE=DYNAMIC
!DYNAMIC
11 , 2
14000, 16000, 20, 15000.0
0.0, 6.6e-5
1, 1, 0.0, 7.2E-7
10, 2, 1
1, 1, 1, 1, 1, 1
!EIGENREAD
eigen_0.log
1, 5
!BOUNDARY
_PickedSet4, 1, 3, 0.0
!FLOAD, LOAD CASE=2
_PickedSet5, 2, 1.
!FLOAD, LOAD CASE=2
_PickedSet6, 2, 1.
!SOLVER,METHOD=CG,PRECOND=1,ITERLOG=NO,TIMELOG=YES
10000, 1
1.0e-8, 1.0, 0.0
!VISUAL,method=PSR
!surface_num=1
!surface 1
!output_type=VTK
!END
Utaratibu wa uchanganuzi¶
Kwanza badilisha data ya udhibiti wa jumla ya modal analysis hecmw_ctrl_eigen.dat kuwa hecmw_ctrl.dat, kisha fanya modal analysis.
Kisha badilisha data ya udhibiti wa jumla ya uchanganuzi wa mwitikio wa masafa hecmw_ctrl_freq.dat kuwa hecmw_ctrl.dat, na ubadilishe faili ya logi ya matokeo ya modal analysis 0.log kuwa eigen_0.log (jina lililobainishwa katika data ya udhibiti wa mwitikio wa masafa), halafu fanya uchanganuzi wa mwitikio wa masafa.
cp hecmw_ctrl_eigen.dat hecmw_ctrl.dat
fistr1 -t 4
mv 0.log eigen_0.log
cp hecmw_ctrl_freq.dat hecmw_ctrl.dat
fistr1 -t 4
Matokeo ya uchanganuzi¶
Uhusiano kati ya frequency na displacement amplitude katika nodi ya ufuatiliaji (nodi 1) iliyobainishwa katika data ya udhibiti umetengenezwa kwa Microsoft Excel na kuonyeshwa katika Mchoro 4.17.3. Pia, sehemu ya faili ya logi ya matokeo imeonyeshwa hapa chini kama data ya nambari ya uchanganuzi.
Log ya matokeo ya uchanganuzi 0.log (frequency-response analysis)¶
fstr_setup: OK
Rayleigh alpha: 0.0000000000000000
Rayleigh beta: 7.1999999999999999E-007
read from=eigen_0.log
start mode= 1
end mode= 5
start frequency: 14000.000000000000
end frequency: 16000.000000000000
number of the sampling points 20
monitor nodeid= 1
14100.000000000000 [Hz] : 8.3935554529723885E-002
14100.000000000000 [Hz] : 1 .res
14200.000000000000 [Hz] : 9.1211083509607632E-002
14200.000000000000 [Hz] : 2 .res
14300.000000000000 [Hz] : 9.9579777896922961E-002
14300.000000000000 [Hz] : 3 .res
14400.000000000000 [Hz] : 0.10914967594967491
14400.000000000000 [Hz] : 4 .res
14500.000000000000 [Hz] : 0.11992223203326918
14500.000000000000 [Hz] : 5 .res
14600.000000000000 [Hz] : 0.13164981801806747
14600.000000000000 [Hz] : 6 .res
14700.000000000000 [Hz] : 0.14360931008440975
14700.000000000000 [Hz] : 7 .res
14800.000000000000 [Hz] : 0.15436500205940235
14800.000000000000 [Hz] : 8 .res
14900.000000000000 [Hz] : 0.16180768408076251
14900.000000000000 [Hz] : 9 .res
15000.000000000000 [Hz] : 0.16388019610373711
15000.000000000000 [Hz] : 10 .res
15100.000000000000 [Hz] : 0.15982110598747551
15100.000000000000 [Hz] : 11 .res
15200.000000000000 [Hz] : 0.15074650286398145
15200.000000000000 [Hz] : 12 .res
15300.000000000000 [Hz] : 0.13885370598993371
15300.000000000000 [Hz] : 13 .res
15400.000000000000 [Hz] : 0.12618976409021948
15400.000000000000 [Hz] : 14 .res
15500.000000000000 [Hz] : 0.11405716994112736
15500.000000000000 [Hz] : 15 .res
15600.000000000000 [Hz] : 0.10306231010139058
15600.000000000000 [Hz] : 16 .res
15700.000000000000 [Hz] : 9.3374567545990342E-002
15700.000000000000 [Hz] : 17 .res
15800.000000000000 [Hz] : 8.4945897112663621E-002
15800.000000000000 [Hz] : 18 .res
15900.000000000000 [Hz] : 7.7641947016103510E-002
15900.000000000000 [Hz] : 19 .res
16000.000000000000 [Hz] : 7.1307642422355627E-002
16000.000000000000 [Hz] : 20 .res
start time: 0.0000000000000000
end time: 6.6000000000000005E-005
frequency: 15000.000000000000
node id: 1
num disp: 10
time= 0.0000000000000000 : 1 .res
time= 0.0000000000000000 : 1 .vis
time= 6.6000000000000003E-006 : 2 .res
time= 6.6000000000000003E-006 : 2 .vis
time= 1.3200000000000001E-005 : 3 .res
time= 1.3200000000000001E-005 : 3 .vis
time= 1.9800000000000000E-005 : 4 .res
time= 1.9800000000000000E-005 : 4 .vis
time= 2.6400000000000001E-005 : 5 .res
time= 2.6400000000000001E-005 : 5 .vis
time= 3.3000000000000003E-005 : 6 .res
time= 3.3000000000000003E-005 : 6 .vis
time= 3.9600000000000000E-005 : 7 .res
time= 3.9600000000000000E-005 : 7 .vis
time= 4.6200000000000005E-005 : 8 .res
time= 4.6200000000000005E-005 : 8 .vis
time= 5.2800000000000003E-005 : 9 .res
time= 5.2800000000000003E-005 : 9 .vis
time= 5.9400000000000000E-005 : 10 .res
time= 5.9400000000000000E-005 : 10 .vis