Civil Engineering Reference
In-Depth Information
α
l
Figure 5.23
m
-coefficients for three pairs of S and
5.4.5.2 Strength of 2-D Elements
The basic equilibrium equations for PC 2-D elements subjected to proportional loadings can
be easily derived by substituting the definitions of the
m
-coefficients (Equations 5.115-5.117),
into the equilibrium equations 1 - 3 of rotating angle theory:
m
σ
1
−
ρ
f
−
ρ
p
f
p
=
σ
d
sin
2
α
r
(5.124)
m
t
σ
1
−
ρ
t
f
t
−
ρ
tp
f
tp
=
σ
d
cos
2
α
r
(5.125)
m
t
σ
1
=
(
−
σ
d
)sin
α
r
cos
α
r
(5.126)
The strength of the element under proportional loadings can be represented by a single stress
σ
1
. This stress
σ
1
can be solved from Equations (5.124)-(5.126) by eliminating the angle
α
r
.
Multiplying Equation (5.124) by Equation (5.125) gives:
−
σ
d
)
2
sin
2
α
r
cos
2
(
m
σ
1
−
ρ
f
−
ρ
p
f
p
)(
m
t
σ
1
−
ρ
t
f
t
−
ρ
tp
f
tp
)
=
(
α
r
(5.127)
Squaring Equation (5.126) gives:
(
m
t
σ
1
)
2
−
σ
d
)
2
sin
2
α
r
cos
2
=
α
r
(
(5.128)
Equating the left-hand sides of Equations (5.127) and (5.128) and rearranging the terms
results in a quadratic equation for
σ
1
as follows:
m
2
2
1
(
m
m
t
−
t
)
σ
−
[
m
(
ρ
t
f
t
+
ρ
tp
f
tp
)
+
m
t
(
ρ
f
+
ρ
p
f
p
)]
σ
1
+
(
ρ
f
+
ρ
p
f
p
)(
ρ
t
f
t
+
ρ
tp
f
tp
)
=
0
(5.129)
=
m
m
t
−
t
m
2
Define
S
(5.130)
B
=
[
m
(
ρ
t
f
t
+
ρ
tp
f
tp
)
+
m
t
(
ρ
f
+
ρ
p
f
p
)]
(5.131)
C
=
(
ρ
f
+
ρ
p
f
p
)(
ρ
t
f
t
+
ρ
tp
f
tp
)
(5.132)