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FIGURE 7.3
Bar of elliptical cross-section.
Introduction of the strains and stresses of Eqs. (1.142) and (1.143) leads to
G ∂ω
z
φ ∂ω
z
x δφ + φ
y +
y δω
y +
V
∂ω
y
φ ∂ω
y dV
x δφ + φ
+
z
z δω
z
+
m x δφ
dx
=
0
(2)
L
This can be separated into two terms that are equal to zero, one containing
δφ
and the other
with
δω
. The
δω
terms appear as
φ 2
y dV
y δω ∂ω
y +
z δω ∂ω
z +
G
y δω
z
z δω
V
y dA
G
L φ 2 dx
y δω ∂ω
y +
z δω ∂ω
=
+
y δω
z
z δω
=
0
(3)
z
A
Thus, the equation that can be solved for
ω
, and that will permit the cross-sectional char-
acteristics to be computed, takes the form
y dA
y δω ∂ω
y +
z δω ∂ω
+
y δω
z
z δω
=
0
(4)
z
A
or
A δω
[
( y ∂∂ y + z ∂∂ z + ( y
z
z
y
)
] dA
=
0
(5)
Suppose the trial solution is
ω = ω
yz
(6)
This volume integral should now be a (cross-sectional) surface integral. Substitution of (6)
in (5) gives
[ z 2
y 2
δω
+
1
) +
1
)
] dA
=
0
(7)
A
or
[ z 2
y 2
+
1
) +
1
)
] dA
=
0
(8)
A
For an ellipse,
z 2 dA
ab 3
y 2 dA
a 3 b
=
π/
4 ,
=
π/
4
A
A
and
ab 3
a 3 b
a 2
b 2
π
π
+
1
) +
1
) =
0or
ω =
(9)
4
4
a 2
+
b 2
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