Civil Engineering Reference
In-Depth Information
T ABLE 16.3
F 1, j L j
Member
L j (mm)
F 1, j
F a, j (N)
AB
4000
1.33
7111.1
700
BC
3000
1.0
3000.0
525
CD
4000
1.33
7111.1
700
DA
3000
1.0
3000.0
525
AC
5000
1.67
13 888.9
875
DB
5000
1.67
13 888.9
875
=
48 000.0
The forces, F a, j , in the members of the complete truss are given in the final column of
Table 16.3.
An alternative approach to the solution of statically indeterminate trusses, both self-
straining and otherwise, is to use the principle of the stationary value of the total
complementary energy. Thus, for the truss of Ex. 16.8, the total complementary energy,
C , is, from Eq. (15.39), given by
F j
n
C
=
δ j d F j
P C
0
j
=
1
in which C is the displacement of the joint C in the direction of P . Let us suppose
that the member BD is short by an amount λ BD (i.e. the lack of fit of BD), then
F j
n
C
=
δ j d F j
P C
X 1 λ BD
0
j
=
1
From the principle of the stationary value of the total complementary energy we have
n
1 δ j F j
C
X 1 =
X 1
λ BD =
0
(16.8)
j
=
Assuming that the truss is linearly elastic, Eq. (16.8) may be written
n
F j L j
A j E j
F j
X 1
C
X 1 =
λ BD =
0
(16.9)
j
=
1
or since, for linearly elastic systems, the complementary energy, C , and the strain
energy, U , are interchangeable,
n
F j L j
A j E j
F j
X 1 =
U
X 1 =
λ BD
(16.10)
j
=
1
Equation (16.10) expresses mathematically what
is generally referred to as
Castigliano's second theorem which states that
 
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