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Slope deflection: B sinks, A rotates

Short answer

By slope-deflection method accounting for support settlement and rotation, the end moments are: M_AB = -1461.18 kNm, M_BA = -494.41 kNm, M_BC = 494.41 kNm, M_CB = 124.26 kNm, M_CD = -124.26 kNm, M_DC = -52.13 kNm.

Analyse the continuous beam shown in figure below by the slope deflection method. Support B sinks by 7.5 mm. Support A rotates by 5° anticlockwise. E=5×105E = 5\times10^{5} MPa, I=3×107 mm4I = 3\times10^{7}\ \text{mm}^4. [Figure: beam ABCD, A fixed; AB = 5 m (1.5I) with 5 kN/m UDL; BC = 2 m + 2 m (2I) with 15 kN at mid-span; CD = 4 m (I) with 5 kN/m UDL; D fixed.]

Data: E=5×105E=5\times10^5 MPa =5×108=5\times10^8 kN/m², I=3×107I=3\times10^7 mm⁴ =3×10−5=3\times10^{-5} m⁴, so EI=15000EI=15000 kNm². AB = 5 m (1.5I) with 5 kN/m; BC = 4 m (2I) with 15 kN at mid-span; CD = 4 m (I) with 5 kN/m. A and D are fixed; support A rotates by 5∘=0.087275^\circ=0.08727 rad anticlockwise and B sinks 7.5 mm.

Support movements

  • θA=−0.08727\theta_A=-0.08727 rad (anticlockwise, so negative in the clockwise-positive convention)
  • ψAB=0.00755=0.00150\psi_{AB}=\dfrac{0.0075}{5}=0.00150, ψBC=−0.00754=−0.00187\psi_{BC}=-\dfrac{0.0075}{4}=-0.00187 (C is higher than B), ψCD=0\psi_{CD}=0

Fixed-end moments (kNm, clockwise +)

  • AB: ∓5×5212=∓10.42\mp\dfrac{5\times5^2}{12}=\mp10.42
  • BC: ∓15×48=∓7.5\mp\dfrac{15\times4}{8}=\mp7.5
  • CD: ∓5×4212=∓6.67\mp\dfrac{5\times4^2}{12}=\mp6.67

Slope-deflection equations

With 2EIL\dfrac{2EI}{L}: AB = 9000, BC = 15000, CD = 7500 kNm/rad.

  • MAB=9000.00(−0.17453+θB)−50.92M_{AB}=9000.00\left(-0.17453 + \theta_{B}\right) - 50.92
  • MBA=9000.00(2θB−0.08727)−30.08M_{BA}=9000.00\left(2\theta_{B} - 0.08727\right) - 30.08
  • MBC=15000.00(2θB+θC)+76.88M_{BC}=15000.00\left(2\theta_{B} + \theta_{C}\right) + 76.88
  • MCB=15000.00(2θC+θB)+91.88M_{CB}=15000.00\left(2\theta_{C} + \theta_{B}\right) + 91.88
  • MCD=7500.00(2θC)−6.67M_{CD}=7500.00\left(2\theta_{C}\right) - 6.67
  • MDC=7500.00(θC)+6.67M_{DC}=7500.00\left(\theta_{C}\right) + 6.67 (The constants include the FEM, the effect of the rotation of A and the chord rotation.)

Equilibrium

Joint B: MBA+MBC=0M_{BA}+M_{BC}=0; joint C: MCB+MCD=0M_{CB}+M_{CD}=0.

[48000.000015000.000015000.000045000.0000]{θBθC}={738.606−85.208}\begin{bmatrix}48000.0000 & 15000.0000 \\ 15000.0000 & 45000.0000\end{bmatrix}\begin{Bmatrix}\theta_{B} \\ \theta_{C}\end{Bmatrix}=\begin{Bmatrix}738.606 \\ -85.208\end{Bmatrix} θB=0.0178374,θC=−0.00783933\theta_{B}=0.0178374,\quad \theta_{C}=-0.00783933

Final end moments (kNm)

EndMM (kNm)EndMM (kNm)
AB-1461.18BA-494.41
BC494.41CB124.26
CD-124.26DC-52.13

Checks:

  • Joint B: (-494.41) + (494.41) = 0.00 kNm (applied clockwise moment 0.00) ✓
  • Joint C: (124.26) + (-124.26) = 0.00 kNm (applied clockwise moment 0.00) ✓

Bending moment diagram ordinates (sagging +, kNm)

MemberBM at first endBM at second endMax within member
AB-1461.18494.41-
BC494.41-124.26-
CD-124.2652.13-

Reactions: A: H=0.00H=0.00, V=403.62V=403.62, M=1461.18M=1461.18; B: H=0.00H=0.00, V=−525.78V=-525.78, M=0.00M=0.00; C: H=0.00H=0.00, V=216.26V=216.26, M=0.00M=0.00; D: H=0.00H=0.00, V=−34.10V=-34.10, M=52.13M=52.13.

The rotation of 5° of support A is very large for a 5 m span, so the end moments are dominated by the support movements.

Answer: MAB=−1461.18M_{AB}=-1461.18, MBA=−494.41M_{BA}=-494.41, MBC=494.41M_{BC}=494.41, MCB=124.26M_{CB}=124.26, MCD=−124.26M_{CD}=-124.26, MDC=−52.13M_{DC}=-52.13 kNm.

✓ Answer checked by Claude Opus 5.5 (high effort)

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