Graphics Programs Reference
In-Depth Information
k i =
/
L ) i , where E is the modulusofelasticity, A represents the cross-
sectional area and L is the length of the member; (2) there aretwocom-
ponents of displacement ateach joint.For the statically indeterminate truss
shown the displacementformulationyields the symmetricequations Ku
( E A
=
p ,
where
.
.
.
.
.
27
58
7
004
7
004
0
0000
0
0000
7
.
004
29
.
57
5
.
253
0
.
0000
24
.
32
K
=
7
.
004
5
.
253
29
.
57
0
.
0000
0
.
0000
MN/m
0
.
0000
0
.
0000
0
.
0000
27
.
58
7
.
004
0
.
0000
24
.
32
0
.
0000
7
.
004
29
.
57
0000
45 T kN
p
=
Determine the displacements u i of the joints.
15.
P 6
P
6
P 5
P 3
P
4
P
P 4
P
45 o
3
45 o
5
P 2
P
P
P
1
2
1
18 kN
12 kN
In the force formulation of a truss, the unknowns are the member forces P i .For
the staticallydeterminate truss shown, the equilibrium equations of the joints
are:
/ 2
11
1
0
0
0
P 1
P 2
P 3
P 4
P 5
P 6
0
18
0
12
0
0
/ 21 0 0
001
/ 2 0
0
1
00
1
/ 2 0
=
00
001
/ 2 1
00
001
2 0
00
0
1
1
/
where the units of P i arekN. (a) Solve the equations as theyare with a computer
program. (b) Rearrange the rows and columnssoastoobtain a lower triangular
coefficient matrix, and then solve the equations by back substitutionusing a
calculator.
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