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(
f 1 =15 : 15 δ 0 1 +1 : 314
f 3 = 476 : 19 δ 0 3 +3
ð6 : 60Þ
Therefore, Eq. (6.59) becomes:
2500
6500 0
2500
0.03
F
6500 43900
4500
6500
x
0
6
=
ð6 : 61Þ
0
4500
750 15.15 0
+
−δ
′′
1.314
1
′′
2500
6500 0
2500 476.19
+
−δ
3
3
Solving for Eq. (6.39) gives:
<
=
<
=
x 6
δ 0 1
δ 0 3
F w
0 : 0093 rad
0 : 0528 m
0 : 0039 m
4 : 8717 MN
=
ð6 : 62Þ
:
;
:
;
(a)
0.0073
0.004
0.004
0.0073
0.0093
0.0 3
l
l
l
l
0.052 8
0 .0039
(b)
0.6589
0.5463
0.2055
0.2055
0.5463 0.6689
0.6589
0.7518
0.7518
0.6589
4.8717
-2.111
2.111
1.25
0.95
0.95
1.25
Figure 6.10 Graphical
illustration of
the response of
the RC frame-shear wall structure.
(a)
Deformations; (b) Internal forces.
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