Civil Engineering Reference
In-Depth Information
6. The equations of step 5 are:
P
m
M
m
ω
1
X
1
=
€
x
1
+ω
P
m
/M
m
X
1
ð
t
Þ =
2
ð
1
−
cos
ω
1
t
Þ
(3.20)
P
m
M
m
ω
2
€
x
2
+ω
2
X
2
=
P
m
/M
m
X
2
ð
t
Þ =
2
ð
1
−
cos
ω
2
t
Þ
(3.21)
P
m
M
m
ω
2
€
x
3
+ω
3
X
3
=
P
m
/M
m
X
3
ð
t
Þ =
2
ð
1
−
cos
ω
3
t
Þ
(3.22)
P
m
M
m
ω
4
X
4
=
P
m
/M
m
X
4
ð
t
Þ =
x
4
+ω
2
ð
1
−
cos
ω
4
t
Þ
(3.23)
8
<
9
=
X
1
X
2
X
3
X
4
= fϕ
1
g
X
1
ð
t
Þ + fϕ
2
g
X
2
ð
t
Þ + fϕ
3
g
X
3
ð
t
Þ + fϕ
4
g
X
4
ð
t
Þ
(3.24)
:
;
Using the above equation, we can define the values of drift with time for each
floor.
3.5.5 In-place Analysis According to ISO 19902
To perform in-place analysis of the load resistance factor design according to
ISO 19902, the general equation for determining the design load (action) (F
d
)
for in-place situations is:
F
d
= γ
f ,G1
G
1
+ γ
f ,G2
G
2
+ γ
f ,Q1
Q
1
+ γ
f ,Q2
Q
2
+ γ
f ,E
o
ð
E
o
+ γ
f ,D
D
o
Þ
+ γ
f ,E
e
ð
E
e
+ γ
f ,D
D
e
Þ
(3.25)
where G
1
and G
2
are the permanent loads; Q
1
and Q
2
are the variable loads; E
o
is the environmental load, which is defined by the owner as the operating wind,
wave and current parameters; D
o
is the equivalent quasi-static action represent-
ing dynamic response, but caused by the wave condition that corresponds with
that for E
o
; E
e
is the extreme quasi-static action due to wind, waves and current;
D
e
is the equivalent quasi-static action representing dynamic response; and
γ
f,G1
,
γ
f,G2
,
γ
f,Q2
are the partial load (action) factors for the various permanent
and variable actions and for which values for different design situations are given
in
Table 3.1
.
On the other hand,
γ
f,Q1
and
γ
f,D
are the partial action factors for the environ-
mental actions and for which appropriate values should be defined by the owner
through the statement of requirement document (SOR),
γ
f,E
and
γ
f,Ee
are partial
action factors applied to the total quasi-static environmental action plus equiva-
lent quasi-static action representing dynamic response for operating and
extreme environmental conditions, respectively, and for which values for differ-
ent design situations are given in
Table 3.1
.
γ
f,Eo
and
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