Skip to main content

Stiffness matrix: frame with 20 kN/m, 10 kN

Short answer

Unknowns θ_B, θ_C, and sway Δ. Fixed-end moments and slope-deflection equations, with storey-shear equilibrium, form a 3×3 stiffness matrix. Solving gives EIθ_B=71.60, EIθ_C=-70.12, EIΔ=5.93. Final end moments (kNm): M_AB=34.32, M_BA=70.12, M_BC=-70.12, M_CB=72.35, M_CD=-72.35, M_DC=-37.28.

Analyse the frame given below using the stiffness matrix method. [Figure: portal frame ABCD; beam BC (2I) of 8 m carrying 20 kN/m UDL with 10 kN horizontal at C; column AB (1.5I) of height 6 m, column CD (I) of height 4 m; A and D fixed.]

Assumptions: A(0,0) and D are fixed; the girder BC (2I, 8 m) is horizontal at the top, AB = 6 m (1.5I) and CD = 4 m (I), so D is 2 m above A. The UDL of 20 kN/m acts downward on BC and the 10 kN load at C acts to the right. Axial deformations are ignored. Take EIEI as the stiffness of I.

Unknown displacements

θB\theta_B, θC\theta_C and the sway Δ\Delta of the girder. Chord rotations: ψAB=Δ/6\psi_{AB}=\Delta/6, ψCD=Δ/4\psi_{CD}=\Delta/4, ψBC=0\psi_{BC}=0.

Fixed-end moments

FEMBC=−20×8212=−106.67FEM_{BC}=-\dfrac{20\times8^2}{12}=-106.67 kNm, FEMCB=+106.67FEM_{CB}=+106.67 kNm. Columns carry no load.

Member stiffness equations

  • MAB=2(1.5EI)6(θB−(0.5000)Δ1)M_{AB}=\frac{2(1.5EI)}{6}\left(\theta_{B} - (0.5000)\Delta_1\right)
  • MBA=2(1.5EI)6(2θB−(0.5000)Δ1)M_{BA}=\frac{2(1.5EI)}{6}\left(2\theta_{B} - (0.5000)\Delta_1\right)
  • MBC=2(2EI)8(2θB+θC)−106.67M_{BC}=\frac{2(2EI)}{8}\left(2\theta_{B} + \theta_{C}\right) - 106.67
  • MCB=2(2EI)8(2θC+θB)+106.67M_{CB}=\frac{2(2EI)}{8}\left(2\theta_{C} + \theta_{B}\right) + 106.67
  • 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 equations

  • Joint B: MBA+MBC=0M_{BA}+M_{BC}=0
  • Joint C: MCB+MCD=0M_{CB}+M_{CD}=0
  • Storey shear: MAB+MBA6+MCD+MDC4+10=0\dfrac{M_{AB}+M_{BA}}{6}+\dfrac{M_{CD}+M_{DC}}{4}+10=0

Combining gives the stiffness matrix equation:

EI[2.00000.5000−0.25000.50002.0000−0.3750−0.2500−0.37500.2708]{θBθCΔ1}={106.667−106.66710.000}EI\begin{bmatrix}2.0000 & 0.5000 & -0.2500 \\ 0.5000 & 2.0000 & -0.3750 \\ -0.2500 & -0.3750 & 0.2708\end{bmatrix}\begin{Bmatrix}\theta_{B} \\ \theta_{C} \\ \Delta_{1}\end{Bmatrix}=\begin{Bmatrix}106.667 \\ -106.667 \\ 10.000\end{Bmatrix}

Typical terms: K11=4(1.5EI)6+4(2EI)8=2EIK_{11}=\dfrac{4(1.5EI)}{6}+\dfrac{4(2EI)}{8}=2EI, K12=2(2EI)8=0.5EIK_{12}=\dfrac{2(2EI)}{8}=0.5EI, K13=−6(1.5EI)62=−0.25EIK_{13}=-\dfrac{6(1.5EI)}{6^2}=-0.25EI (sign convention of the rows above, positive sway to the right).

Solution

EIθB=71.6049,EIθC=−70.1235,EIΔ1=5.9259EI\theta_{B}=71.6049,\quad EI\theta_{C}=-70.1235,\quad EI\Delta_{1}=5.9259

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

EndMM (kNm)EndMM (kNm)
AB34.32BA70.12
BC-70.12CB72.35
CD-72.35DC-37.28

Checks:

  • Joint B: (70.12) + (-70.12) = 0.00 kNm (applied clockwise moment 0.00) ✓
  • Joint C: (72.35) + (-72.35) = 0.00 kNm (applied clockwise moment 0.00) ✓
  • Storey shear: 104.446+−109.634+10=0.00\dfrac{104.44}{6}+\dfrac{-109.63}{4}+10=0.00 ✓
MemberBM at first endBM at second endMax within member
AB34.32-70.12-
BC-70.12-72.3588.77 at 3.99 m
CD-72.3537.28-

Reactions: A: H=17.41H=17.41, V=79.72V=79.72, M=−34.32M=-34.32; D: H=−27.41H=-27.41, V=80.28V=80.28, M=37.28M=37.28.

Answer: MAB=34.32M_{AB}=34.32, MBA=70.12M_{BA}=70.12, MBC=−70.12M_{BC}=-70.12, MCB=72.35M_{CB}=72.35, MCD=−72.35M_{CD}=-72.35, MDC=−37.28M_{DC}=-37.28 kNm.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Theory of Structures II chapter 3 questions →