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Table 6. Non-dimensional damping ratios γ i
Uniform distribution of dampers
Optimal distribution of dampers
Mode
Number
Frame without
dampers
Kelvin model
Maxwell model
Kelvin model
Maxwell model
1
0.0008
0.0038
0.0036
0.0043
0.0049
2
0.0022
0.0099
0.0087
0.0085
0.0139
3
0.0035
0.0137
0.0113
0.0107
0.0148
4
0.0047
0.0162
0.0129
0.0118
0.0094
5
0.0061
0.0231
0.0177
0.0181
0.0251
6
0.0066
0.0195
0.0143
0.0200
0.0150
7
0.0073
0.0219
0.0157
0.0261
0.0218
8
0.0085
0.0208
0.0151
0.0237
0.0230
9
0.0097
0.0209
0.0154
0.0228
0.0111
10
0.0112
0.0212
0.0160
0.0214
0.0112
12a). The assumed values of the sum of the
damping coefficients and the sum of the stiffness
parameters are: C d = 500 kNsec / α , and
K d = 25000 kNm 2 , respectively. If dampers
are uniformly distributed within a structure, then
the data for every single damper are:
k d = 2500 kNm 2 , c d = 50 kNsec /m
= = kN/m ,
but the mass value is the same for every floor:
m s = 2 07
k
k
16450
9
10
.
Mg . The structure's damping factors
are:
c
= = .
c
4 76
kNsec/m
1
2
c c
3
= = .
3 73
kNsec/m
4
c
= = .
c
2 91
kNsec/m
α
,
5
6
c
= = .
c
1 98
kNsec/m
c = / 0 02 . The values of fractional
parameters for all dampers are identical, i.e.,
α = 0 . . The above values of damper param-
eters are used for both of the considered frac-
tional models. Using the suggested procedure,
the dynamic properties of the considered system
were computed (see Table 6). These results show
that a frame with uniformly distributed dampers
is less damped by the fractional Maxwell damp-
er than by the fractional Kelvin damper if both
dampers have identical values of parameters.
The optimization procedures provide lower
values of damping ratios in the case of the Kel-
vin model of damper for the first, second, third
and fifth modes of vibration in comparison with
the Maxwell model. But the results of optimiza-
tion correspond to the different dampers distribu-
tion at frame structure (see Table 6 and Figure
12).
τ d
7
8
d
d
c c
9
= = . kNsec/m .
The data is taken from Zhang and Soong (1992).
Two rheological models describing the dynamic
behaviour of dampers were applied in the calcu-
lations; the Kelvin fractional model and the
Maxwell fractional model.
Firstly, the calculations were carried out for a
frame without dampers, only the damping proper-
ties of the structure were taken into account. The
solution to Equation (44), where A
1 44
10
1 = and
K dd = 0 , leads to the eigenvalues s i which enables
determination of the dynamic properties of the
structure described by Equation (28). The results,
the natural frequencies of the structure and the
values of non-dimensional damping ratios are
presented in Table 5 and in the second column of
Table 6, respectively.
Next, the authors investigated a structure with
one damper mounted on every storey (see Figure
0
 
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