- 2072 Kartik · 10 marks
Stiffness matrix: frame, flexural deformations only
Short answer
Stiffness matrix method considering flexural deformations: unknowns θ_B, θ_C and sway Δ; final end moments are M_AB = -41.70, M_BA = -7.18, M_BC = 7.18, M_CB = 20.34, M_CD = -5.34, M_DC = -13.29 kNm.
Analyse the frame shown in figure using the stiffness matrix method. Consider only flexural deformations. [Figure: frame; left column 2EI with 15 kN/m UDL horizontally; beam EI of 3 m + 2 m with 10 kN downward load and 15 kNm moment; right column EI of height 2 m + 1 m, fixed base.]
Assumptions (figure partly illegible): A(0,0), B(0,3), C(5,3), D(5,0): both columns are 3 m high (left column AB = 2EI, right column CD = EI), the beam BC = 5 m (EI). The 15 kN/m load acts horizontally to the right on AB, the 10 kN load acts downward at 3 m from B and the 15 kNm moment at C is clockwise. A and D are fixed. Only flexural deformation is considered (axial and shear deformations are neglected).
Unknowns
and the sway of the beam: .
Fixed-end moments (clockwise +)
- AB: kNm, with the sign for a horizontal load on a vertical member: , kNm
- BC (, ): , kNm
Stiffness equations of the members
Equilibrium
- Joint B:
- Joint C:
- Storey shear: the 15 kN/m load on AB is replaced by its fixed-end reaction at the girder level (the fixed-end shear kN at B), giving the sway equation with right-hand side 22.50 kN.
Final end moments (kNm, clockwise +)
| End | (kNm) | End | (kNm) |
|---|---|---|---|
| AB | -41.70 | BA | -7.18 |
| BC | 7.18 | CB | 20.34 |
| CD | -5.34 | DC | -13.29 |
Checks:
- Joint B: (-7.18) + (7.18) = 0.00 kNm (applied clockwise moment 0.00) ✓
- Joint C: (20.34) + (-5.34) = 15.00 kNm (applied clockwise moment 15.00) ✓
| Member | BM at first end | BM at second end | Max within member |
|---|---|---|---|
| AB | -41.70 | 7.18 | 8.46 at 2.59 m |
| BC | 7.18 | -20.34 | - |
| CD | -5.34 | 13.29 | - |
Reactions: A: , , ; D: , , .
Answer: , , , , , kNm.
✓ Answer checked by Claude Opus 5.5 (high effort)
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