Civil Engineering Reference
In-Depth Information
1
(
)
()
*
T
where
S
ω
=
lim
a
is the cross spectral density matrix of the modal
a
RR
R
R
π
T
T
→∞
()
t
buffeting wind load.
R
is given in Eq. 9.111, and thus
N
N
()
T
()
T
T
()
T
T
()
ˆ
R Φ R Φ
t
t
AR Φ
t
ABψ v
t
=
=
=
(9.155)
nn
n Qnn
n
n
1
n
1
=
=
Taking the Fourier transform throughout Eq. 9.155 renders
N
()
T
T
n
()
a
ω
=⋅
Φ
ABψ a
ω
(9.156)
Qn
v
ˆ
R
n
n
n
1
=
and thus, the cross spectral density matrix of the modal buffeting wind load is given by
T
N
N
⎤ ⎡
1
(
)
(
)
()
T
T
*
ˆ
T
T
lim
S
ω
=
Φ ABψ a
Φ ABψ a
⎥ ⎢
ˆ
nQnv
nQnv
RR
T
n
n
n
n
π
T
→∞
⎦ ⎣
n
1
n
1
=
=
NN
1
(
)
T
∑∑
T
*
ˆ
T
T
T
lim
=
Φ
ABψ
aa ψ BAΦ
(9.157)
nQn
v v
ˆ
mQ
m
n
T
n
m
m
π
T
→∞
nm
==
11
NN
ˆ
T
∑∑
T
()
T
T
=⋅
Φ
ABψ S
ω
ψ BA
Φ
n
Qn
vv
ˆˆ
mQ
m
n
m
nm
11
==
1
(
)
ˆ
()
*
T
where
S
ω
=
lim
a
a
is the cross spectral density matrix of the reduced
vv
ˆˆ
v
ˆ
nm
ˆ
π
T
T
→∞
turbulence velocity vector, previously developed in chapter 9.6, see Eq. 9.124. Thus
()
*
()
()
T
()
*
()
T
()
T
()
S
ω
=
H
ω
S
ω
H
ω
=
H
ω
Φ S
ω
Φ H
ω
RR
ηη
η
RR
η
η
η
(9.158)
NN
(
)
ˆ
ˆ
ˆ
*
T
∑∑
T
1 2
1 2
T
T
T
=
H Φ
ABψ SCo S ψ BAΦ H
η
nnn n mm
mmm
η
nm
11
==
ˆ
ˆ n
ˆ m
(
)
()
()
s
,
where
Co
Δ
ω
,
S
ω
and
S
ω
are defined in Eqs. 9.120 and 9.121.
nm
nm
()
()
()
()
Finally, since
r Φη , then
t
=⋅
t
a
ω
=⋅
Φ a
ω
, and thus, the cross spectral
r
η
density matrix of the displacement response quantities is given by
 
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