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Stiffness matrix: frame with 50 kNm moment

Short answer

Using stiffness matrix for unknowns θ_B, θ_C and sway Δ, solving joint and storey equilibrium gives end moments: M_AB = –44.92, M_BA = –1.08, M_BC = 1.08, M_CB = 96.42, M_CD = –46.42, M_DC = –67.58 kNm (clockwise positive); EIΔ = 236.67 kNm³.

Analyse the given frame using the stiffness matrix method. [Figure: portal frame ABCD, columns AB and CD of height 4 m with EI, beam BC span 8 m with EI carrying 10 kN/m UDL; 40 kN horizontal at B; 50 kNm moment applied at C; A and D fixed.]

Assumptions: the 10 kN/m UDL acts downward on BC, the 40 kN load at B acts to the right and the 50 kNm moment at C is clockwise. EI is constant, axial deformation is neglected, A and D are fixed.

Degrees of freedom

θB,θC\theta_B,\theta_C (joint rotations, clockwise +) and Δ\Delta (horizontal sway of beam BC, right +). Since BC is axially rigid, B and C move equally, so ψAB=ψCD=Δ/4\psi_{AB}=\psi_{CD}=\Delta/4 and ψBC=0\psi_{BC}=0.

Member relation: Mij=2EIL(2θi+θj−3ψ)+FEMijM_{ij}=\dfrac{2EI}{L}(2\theta_i+\theta_j-3\psi)+FEM_{ij} (clockwise end moments +).

Fixed-end moments

FEMBC=−wL212=−10×8212=−53.33FEM_{BC}=-\dfrac{wL^2}{12}=-\dfrac{10\times8^2}{12}=-53.33 kNm, FEMCB=+53.33FEM_{CB}=+53.33 kNm. The columns carry no load between joints, so their FEMs are zero.

Stiffness equations for the members

  • MAB=2EI4(θB−(0.7500)Δ1)M_{AB}=\frac{2EI}{4}\left(\theta_{B} - (0.7500)\Delta_1\right)
  • MBA=2EI4(2θB−(0.7500)Δ1)M_{BA}=\frac{2EI}{4}\left(2\theta_{B} - (0.7500)\Delta_1\right)
  • MBC=2EI8(2θB+θC)−53.33M_{BC}=\frac{2EI}{8}\left(2\theta_{B} + \theta_{C}\right) - 53.33
  • MCB=2EI8(2θC+θB)+53.33M_{CB}=\frac{2EI}{8}\left(2\theta_{C} + \theta_{B}\right) + 53.33
  • MCD=2EI4(2θC−(0.7500)Δ1)M_{CD}=\frac{2EI}{4}\left(2\theta_{C} - (0.7500)\Delta_1\right)
  • MDC=2EI4(θC−(0.7500)Δ1)M_{DC}=\frac{2EI}{4}\left(\theta_{C} - (0.7500)\Delta_1\right)

Equilibrium conditions

  • Joint B: MBA+MBC=0M_{BA}+M_{BC}=0
  • Joint C: MCB+MCD=50M_{CB}+M_{CD}=50 (the applied clockwise moment)
  • Storey shear: the column shears resist the 40 kN load, MAB+MBA4+MCD+MDC4+40=0\dfrac{M_{AB}+M_{BA}}{4}+\dfrac{M_{CD}+M_{DC}}{4}+40=0

Substituting the member equations gives [K]{d}={F}[K]\{d\}=\{F\}:

EI[1.50000.2500−0.37500.25001.5000−0.3750−0.3750−0.37500.3750]{θBθCΔ1}={53.333−3.33340.000}EI\begin{bmatrix}1.5000 & 0.2500 & -0.3750 \\ 0.2500 & 1.5000 & -0.3750 \\ -0.3750 & -0.3750 & 0.3750\end{bmatrix}\begin{Bmatrix}\theta_{B} \\ \theta_{C} \\ \Delta_{1}\end{Bmatrix}=\begin{Bmatrix}53.333 \\ -3.333 \\ 40.000\end{Bmatrix}

(First two rows: joint B and C. Third row: sway equation. The load vector holds the applied loads minus the fixed-end effects.)

Solution

EIθB=87.6667,EIθC=42.3333,EIΔ1=236.6667EI\theta_{B}=87.6667,\quad EI\theta_{C}=42.3333,\quad EI\Delta_{1}=236.6667

Final end moments (kNm, clockwise on the member end +)

EndMM (kNm)EndMM (kNm)
AB-44.92BA-1.08
BC1.08CB96.42
CD-46.42DC-67.58

Checks:

  • Joint B: (-1.08) + (1.08) = 0.00 kNm (applied clockwise moment 0.00) ✓
  • Joint C: (96.42) + (-46.42) = 50.00 kNm (applied clockwise moment 50.00) ✓
  • Storey shear: (−46.00)+(−114.00)4+40=0.00\dfrac{(-46.00)+(-114.00)}{4}+40=0.00 ✓

Bending moment diagram ordinates (sagging/inside tension +, kNm)

MemberBM at first endBM at second endMax within member
AB-44.921.08-
BC1.08-96.4239.76 at 2.78 m
CD-46.4267.58-

Reactions: A: H=−11.50H=-11.50, V=27.81V=27.81, M=44.92M=44.92; D: H=−28.50H=-28.50, V=52.19V=52.19, M=67.58M=67.58 (M anticlockwise +).

Answer: MAB=−44.92M_{AB}=-44.92, MBA=−1.08M_{BA}=-1.08, MBC=1.08M_{BC}=1.08, MCB=96.42M_{CB}=96.42, MCD=−46.42M_{CD}=-46.42, MDC=−67.58M_{DC}=-67.58 kNm; sway EIΔ=236.67EI\Delta=236.67.

✓ Answer checked by Claude Opus 5.5 (high effort)

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