410 11 Matrix Stiffness Method
Vector of internal unknowns bending moments isESfinDSE 1 CSE 2 ,where
SE 2 DkAQ TZEDEI
5
2
6
6
4
4200
2400
0030
0005
3
7
7
5
2
6
6
4
0 0:2
1 0:2
10
1 0:333
3
7
7
5
1
EI
3:7944
22:452
D
2 6 6 6 6 6
3:8707
2:3529
2:2766
11:2709
3 7 7 7 7 7
Control:ASDEP. In our case
0111
0:20:2 0 0:333
2 6 6 6 6 6
3:8707
2:3529
2:2766
11:2709
3 7 7 7 7 7
D
11:1946
4:9979
Final bending moments at specified sections 1–4 are
SEfinDES 1 CSE 2 D
2 6 6 6 6 6
4:1667
4:1667
15:36
0
3 7 7 7 7 7
C
2 6 6 6 6 6
3:8707
2:3529
2:2766
11:2709
3 7 7 7 7 7
D
2 6 6 6 6 6
8:0374
1:8138
13:0834
11:2709
3 7 7 7 7 7
This vector allows us to construct the bending moment diagram. All ordi-
nates should be plotted according S-e diagram (Fig.11.27d). For example,
M 1 D8:037kNm should be plotted at the supportAleft at neutral line. Final
bending moment diagram is presented in Fig. 8.2g. Note that stiffness matrix method
is precise and some disagreement with data obtained previously is a result of the
rounding off.
11.8 Analysis of Statically Indeterminate Trusses.........................
Figure11.28a presents the statically indeterminate truss; the stiffnessEAfor all
members is equal. We need to compute the displacements of the all joints, and cal-
culate the internal forces.
First let us construct theZ-Pdiagram (Fig.11.28b). This diagram shows possible
joint displacements and corresponding possible loads. After that we can construct
the vector of external forces
PED^0 4 200 ̆T: