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Slope deflection: D rotates, C settles 4 mm

Short answer

Slope-deflection with support settlement and rotation gives M_BA=75, M_BC=-75, M_CB=-18.43, M_CD=18.43, M_DC=117.75 kNm for EI=30,000 kNm². General form includes load and movement terms.

Analyse the beam shown in figure below by the slope deflection method. Draw BM diagram considering given external loading and rotation of support D by (1/10) clockwise, support C settles down by 4 mm. [Figure: beam ABCD, D fixed; 25 kN at the free end A; AB = 3 m (EI); BC = 2 m + 2 m + 2 m (2.5EI) with 50 kN and 40 kN point loads and 10 kN/m UDL on the right part of BC; CD = 3 m + 3 m (3EI).]

Data and assumptions: the figure is only described. A is the free end of the cantilever AB (3 m, 25 kN at A); BC = 6 m (2.5EI) carries 50 kN at 2 m and 40 kN at 4 m from B and 10 kN/m over the last 2 m; CD = 6 m (3EI) is unloaded; B and C are supports; D is fixed. Support C settles 4 mm; support D rotates 110\tfrac{1}{10} degree =0.001745=0.001745 rad clockwise (the unit is taken as degrees). EI is not given, so the answer is split into the load part (independent of EI) and the support-movement part (proportional to EI), and a numerical example with EI=30 000EI=30\,000 kNm² is worked out.

Step 1: Overhang AB

MB=25×3=75M_B=25\times3=75 kNm (hogging), known moment at B.

Step 2: Fixed-end moments (kNm, clockwise +)

BC: 50 kN at a=2a=2 (b=4b=4), 40 kN at a=4a=4 (b=2b=2) and UDL on the last 2 m: FEMBC=−65.556FEM_{BC}=-65.556, FEMCB=70.000FEM_{CB}=70.000 (sum of the point-load formulas ∓Pab2/L2\mp Pab^2/L^2, ±Pa2b/L2\pm Pa^2b/L^2 and the integrated UDL contribution). CD: 0.

Step 3: Support movement

  • ψBC=+0.0046=0.000667\psi_{BC}=+\dfrac{0.004}{6}=0.000667 (C moves down relative to B, so the chord of BC turns clockwise) and ψCD=−0.0046=−0.000667\psi_{CD}=-\dfrac{0.004}{6}=-0.000667 (D is higher than C, so the chord of CD turns anticlockwise); ψAB\psi_{AB} does not enter (overhang).
  • θD=+0.001745\theta_D=+0.001745 rad (clockwise) appears in MCDM_{CD} and MDCM_{DC}.

Step 4: Slope-deflection equations (EI=30 000EI=30\,000 kNm², numerical)

  • MBC=25000.00(2θB+θC)−115.56M_{BC}=25000.00\left(2\theta_{B} + \theta_{C}\right) - 115.56
  • MCB=25000.00(2θC+θB)+20.00M_{CB}=25000.00\left(2\theta_{C} + \theta_{B}\right) + 20.00
  • MCD=30000.00(2θC+0.00175)+60.00M_{CD}=30000.00\left(2\theta_{C} + 0.00175\right) + 60.00
  • MDC=30000.00(0.00349+θC)+60.00M_{DC}=30000.00\left(0.00349 + \theta_{C}\right) + 60.00

Step 5: Equilibrium and solution

Joint B: MBC=−MBAM_{BC}=-M_{BA} with MBA=+75M_{BA}=+75, so MBC=−75M_{BC}=-75. Joint C: MCB+MCD=0M_{CB}+M_{CD}=0.

[50000.000025000.000025000.0000110000.0000]{θBθC}={40.556−132.360}\begin{bmatrix}50000.0000 & 25000.0000 \\ 25000.0000 & 110000.0000\end{bmatrix}\begin{Bmatrix}\theta_{B} \\ \theta_{C}\end{Bmatrix}=\begin{Bmatrix}40.556 \\ -132.360\end{Bmatrix} θB=0.00159387,θC=−0.00156551\theta_{B}=0.00159387,\quad \theta_{C}=-0.00156551

Step 6: Final end moments (kNm)

EndLoads only (EI-independent)Support movements, per unit EITotal for EI = 30 000
BA75.00-0.00000075.00
BC-75.00-0.000000-75.00
CB40.17-0.001953-18.43
CD-40.170.00195318.43
DC-20.090.004595117.75

(The middle column multiplied by EI gives the effect of the movements for any EI: M=Mload+EI×(column 3)M=M_{load}+EI\times(\text{column 3}).)

Check: joint B: 75.00+(−75.00)=075.00+(-75.00)=0 ✓; joint C: −18.43+(18.43)=0-18.43+(18.43)=0 ✓.

Bending moment diagram (EI = 30 000)

MemberBM at first endBM at second endMax within member
AB0.00-75.00-
BC-75.0018.4387.29 at 4.00 m
CD18.43-117.75-

Reactions: B: H=0.00H=0.00, V=90.57V=90.57, M=0.00M=0.00; C: H=0.00H=0.00, V=21.73V=21.73, M=0.00M=0.00; D: H=0.00H=0.00, V=22.70V=22.70, M=−117.75M=-117.75.

Answer: for EI=30 000EI=30\,000 kNm²: MBA=75.00M_{BA}=75.00, MBC=−75.00M_{BC}=-75.00, MCB=−18.43M_{CB}=-18.43, MCD=18.43M_{CD}=18.43, MDC=117.75M_{DC}=117.75 kNm; in general M=Mload+EI×(movement coefficient)M=M_{load}+EI\times(\text{movement coefficient}).

✓ Answer checked by Claude Opus 5.5 (high effort)

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