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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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