- 2070 Asar · 10 marks
Stiffness matrix: continuous beam BMD
Short answer
Using theta_B and theta_C, solve EI[[1.0714,0.25],[0.25,0.5]]{theta}={-9.694,-55}. Final moments are M_AB=-17.07, M_BA=45.44, M_BC=-45.44, M_CB=0 kNm; maximum sagging in BC is 51.53 kNm at 5.38 m from B.
Analyse the continuous beam and draw bending moment diagram which is loaded as shown in figure below. Use the stiffness matrix method. [Figure: beam ABC, A fixed; 10 kN at 2 m and 30 kN at 5 m from A; B support at 7 m (2 m + 3 m + 2 m); BC = 8 m (4 m + 4 m) with 15 kN/m UDL on the right 4 m; C roller.]
Data: A is fixed; AB = 7 m with 10 kN at 2 m and 30 kN at 5 m from A; B is a roller support; BC = 8 m with 15 kN/m on the right-hand 4 m (from 4 m to 8 m from B); C is a roller (free to rotate). EI is constant.
Unknown displacements (coordinates)
1 = , 2 = (clockwise +). and there are no support settlements.
Fixed-end moments (clockwise +, kNm)
- AB (point loads): load 10 kN (, ): = , ; load 30 kN (, ): , . Total: , .
- BC (partial UDL, 15 kN/m over 4 m, from the right end): , (integration of the point-load formulas over the loaded length).
Member stiffness equations
Stiffness matrix equation ()
The roller C gives and the joint B gives :
, , .
Final end moments (kNm)
| End | (kNm) | End | (kNm) |
|---|---|---|---|
| AB | -17.07 | BA | 45.44 |
| BC | -45.44 | CB | 0.00 |
Checks: Joint B: ✓; roller C: ✓.
Bending moment diagram (sagging +, kNm)
| Member | BM at first end | BM at second end | Max within member |
|---|---|---|---|
| AB | -17.07 | -45.44 | 11.23 at 5.00 m |
| BC | -45.44 | 0.00 | 51.53 at 5.38 m |
| BM under the 10 kN load: 6.25; under the 30 kN load: 11.23 kNm. |
Reactions: A: , , ; B: , , ; C: , , .
Answer: , , kNm, ; maximum sagging in BC = 51.53 kNm at 5.38 m from B.
✓ Answer checked by Claude Opus 5.5 (high effort)
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