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Stiffness method: frame with 16 t, 5 t

Short answer

Kinematic unknowns θB, θC, sway Δ. Solving equilibrium gives EIθB=10.64, EIθC=-9.32, EIΔ=27.20; member end moments: M_AB=-11.05, M_BA=-3.95, M_BC=3.95, M_CB=0 t·m.

Analyze the frame given below with inextensible members using the stiffness method. [Figure: frame; column AB (I) of 3 m + 2 m + 2 m heights with 5 t horizontal load; beam BC (2I) of 4 m (2 m + 2 m) with 16 t vertical load at mid-span; C on a roller; A fixed.]

Assumptions

Column AB is 3 m high, with the 5 t horizontal load at joint B. Beam BC is 4 m with the 16 t load at its mid-point. Units: t and m. Axial deformation is ignored (inextensible), so B and C move horizontally by the same sway Δ\Delta and neither joint moves vertically.

Degrees of freedom

Unknowns: θB\theta_B, θC\theta_C and the sway Δ\Delta (chord rotation of the column ψ=Δ/3\psi = \Delta/3). Kinematic indeterminacy = 3. Clockwise end moments are positive.

Fixed-end moments

BC: PL/8=16×4/8=8PL/8 = 16\times 4/8 = 8 t·m, so FEMBC=−8FEM_{BC} = -8, FEMCB=+8FEM_{CB} = +8.

Stiffness (slope-deflection) equations

MAB=2EI3 (θB−3ψ)=2EI3θB−2EI3ΔMBA=2EI3 (2θB−3ψ)=4EI3θB−2EI3ΔMBC=2(2EI)4(2θB+θC)−8=EI(2θB+θC)−8MCB=EI(θB+2θC)+8\begin{aligned} M_{AB} &= \tfrac{2EI}{3}\,(\theta_B - 3\psi) = \tfrac{2EI}{3}\theta_B - \tfrac{2EI}{3}\Delta \\ M_{BA} &= \tfrac{2EI}{3}\,(2\theta_B - 3\psi) = \tfrac{4EI}{3}\theta_B - \tfrac{2EI}{3}\Delta \\ M_{BC} &= \tfrac{2(2EI)}{4}(2\theta_B + \theta_C) - 8 = EI(2\theta_B+\theta_C) - 8 \\ M_{CB} &= EI(\theta_B + 2\theta_C) + 8 \end{aligned}

Equilibrium equations

  1. Joint B: MBA+MBC=0M_{BA} + M_{BC} = 0
  2. Joint C (roller, no moment): MCB=0M_{CB} = 0
  3. Horizontal force: the only horizontal restraint is at A, so the column shear equals the 5 t load: (MAB+MBA)/3=−5(M_{AB} + M_{BA})/3 = -5

Substituting:

103EI θB+EI θC−23EI Δ=8EI θB+2EI θC=−82EI θB−43EI Δ=−15\begin{aligned} \tfrac{10}{3}EI\,\theta_B + EI\,\theta_C - \tfrac{2}{3}EI\,\Delta &= 8 \\ EI\,\theta_B + 2EI\,\theta_C &= -8 \\ 2EI\,\theta_B - \tfrac{4}{3}EI\,\Delta &= -15 \end{aligned}

Solving:

EI θB=11711=10.636,EI θC=−20522=−9.318,EI Δ=119744=27.205EI\,\theta_B = \tfrac{117}{11} = 10.636,\quad EI\,\theta_C = -\tfrac{205}{22} = -9.318,\quad EI\,\Delta = \tfrac{1197}{44} = 27.205

Member end moments

EndMoment (t·m)
MABM_{AB}-11.045 (anticlockwise)
MBAM_{BA}-3.955
MBCM_{BC}+3.955
MCBM_{CB}0

Joint B: −3.955+3.955=0-3.955 + 3.955 = 0 (check).

Reactions and diagrams

  • Reaction at C (moments about B for beam BC, with MBC=3.955M_{BC} = 3.955 clockwise): RC=(16×2+3.955)/4=8.989R_C = (16\times 2 + 3.955)/4 = 8.989 t up.
  • At A: VA=16−8.989=7.011V_A = 16 - 8.989 = 7.011 t up, HA=5H_A = 5 t to the left, MA=11.045M_A = 11.045 t·m anticlockwise.
  • BMD: column AB is a straight line from 11.045 at A, passing through zero 2.21 m above A, to 3.955 at B on the opposite face. Beam BC: 3.955 (sagging) at B, 17.977 sagging under the 16 t load, 0 at C.
  • SFD: column 5 t constant; beam +7.011 from B up to the load, then -8.989 to C.
  • Axial: column AB carries 7.011 t compression; beam BC has no axial force.

Answer: θB=10.64/EI\theta_B = 10.64/EI, θC=−9.32/EI\theta_C = -9.32/EI, Δ=27.20/EI\Delta = 27.20/EI; MAB=−11.05M_{AB}=-11.05, MBA=−3.95M_{BA}=-3.95, MBC=3.95M_{BC}=3.95, MCB=0M_{CB}=0 t·m.

✓ Answer checked by Claude Opus 5.5 (high effort)

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