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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

θB,θC\theta_B,\theta_C and the sway Δ\Delta of the beam: ψAB=ψCD=Δ/3\psi_{AB}=\psi_{CD}=\Delta/3.

Fixed-end moments (clockwise +)

  • AB: ∓wL212=∓15×3212=∓11.25\mp\dfrac{wL^2}{12}=\mp\dfrac{15\times3^2}{12}=\mp11.25 kNm, with the sign for a horizontal load on a vertical member: FEMAB=−11.25FEM_{AB}=-11.25, FEMBA=11.25FEM_{BA}=11.25 kNm
  • BC (a=3a=3, b=2b=2): FEMBC=−10×3×2252=−4.80FEM_{BC}=-\dfrac{10\times3\times2^2}{5^2}=-4.80, FEMCB=+10×32×252=7.20FEM_{CB}=+\dfrac{10\times3^2\times2}{5^2}=7.20 kNm

Stiffness equations of the members

  • MAB=2(2EI)3(θB−(1.0000)Δ1)−11.25M_{AB}=\frac{2(2EI)}{3}\left(\theta_{B} - (1.0000)\Delta_1\right) - 11.25
  • MBA=2(2EI)3(2θB−(1.0000)Δ1)+11.25M_{BA}=\frac{2(2EI)}{3}\left(2\theta_{B} - (1.0000)\Delta_1\right) + 11.25
  • MBC=2EI5(2θB+θC)−4.80M_{BC}=\frac{2EI}{5}\left(2\theta_{B} + \theta_{C}\right) - 4.80
  • MCB=2EI5(2θC+θB)+7.20M_{CB}=\frac{2EI}{5}\left(2\theta_{C} + \theta_{B}\right) + 7.20
  • MCD=2EI3(2θC−(1.0000)Δ1)M_{CD}=\frac{2EI}{3}\left(2\theta_{C} - (1.0000)\Delta_1\right)
  • MDC=2EI3(θC−(1.0000)Δ1)M_{DC}=\frac{2EI}{3}\left(\theta_{C} - (1.0000)\Delta_1\right)

Equilibrium

  • Joint B: MBA+MBC=0M_{BA}+M_{BC}=0
  • Joint C: MCB+MCD=15M_{CB}+M_{CD}=15
  • Storey shear: the 15 kN/m load on AB is replaced by its fixed-end reaction at the girder level (the fixed-end shear wL/2=22.5wL/2=22.5 kN at B), giving the sway equation with right-hand side 22.50 kN.
EI[3.46670.4000−1.33330.40002.1333−0.6667−1.3333−0.66671.3333]{θBθCΔ1}={−6.4507.80022.500}EI\begin{bmatrix}3.4667 & 0.4000 & -1.3333 \\ 0.4000 & 2.1333 & -0.6667 \\ -1.3333 & -0.6667 & 1.3333\end{bmatrix}\begin{Bmatrix}\theta_{B} \\ \theta_{C} \\ \Delta_{1}\end{Bmatrix}=\begin{Bmatrix}-6.450 \\ 7.800 \\ 22.500\end{Bmatrix} EIθB=9.0133,EIθC=11.9186,EIΔ1=31.8476EI\theta_{B}=9.0133,\quad EI\theta_{C}=11.9186,\quad EI\Delta_{1}=31.8476

Final end moments (kNm, clockwise +)

EndMM (kNm)EndMM (kNm)
AB-41.70BA-7.18
BC7.18CB20.34
CD-5.34DC-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) ✓
MemberBM at first endBM at second endMax within member
AB-41.707.188.46 at 2.59 m
BC7.18-20.34-
CD-5.3413.29-

Reactions: A: H=−38.79H=-38.79, V=−1.50V=-1.50, M=41.70M=41.70; D: H=−6.21H=-6.21, V=11.50V=11.50, M=13.29M=13.29.

Answer: MAB=−41.70M_{AB}=-41.70, MBA=−7.18M_{BA}=-7.18, MBC=7.18M_{BC}=7.18, MCB=20.34M_{CB}=20.34, MCD=−5.34M_{CD}=-5.34, MDC=−13.29M_{DC}=-13.29 kNm.

✓ Answer checked by Claude Opus 5.5 (high effort)

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