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Slope deflection: B sinks, C rotates

Short answer

Using slope-deflection with given settlement and rotation, equilibrium gives θB = -0.0055125 rad. For EI=20000 t m², end moments: AB=-94.88, BA=-147.00, BC=147.00, CB=499.17 tm. General: M=Mload+EI×coefficient.

Determine the member end moments using the slope deflection method and draw BMD and SFD for the beam loaded as shown in figure given below. Support B settles down by 5 mm and support C rotates clockwise by 0.02 radian and EI=20 t/mm2EI = 20\ \text{t/mm}^2. [Figure: beam A-B-C, A fixed, B support, C fixed; 4 t point load at 1 m from A; AB = 1 m + 3 m (I); BC = 6 m (2I) with 2 t/m UDL.]

Data and assumptions: A is fixed; AB = 1 m + 3 m = 4 m (I) with 4 t at 1 m from A; BC = 6 m (2I2I) with 2 t/m; C is fixed. Support B settles 5 mm and support C rotates 0.02 rad clockwise. The value 'EI = 20 t/mm²' gives only E (20 t/mm² =2×107=2\times10^7 t/m²); I is not given. The result is therefore written as: moment = (load part, independent of EI) + EI × (settlement/rotation part), and a numerical example with I=1×10−3I=1\times10^{-3} m⁴ (EI=20 000EI=20\,000 t m²) is given. Units: tonne, metre.

Step 1: Chord rotations and support rotation

  • ψAB=0.0054=0.001250\psi_{AB}=\dfrac{0.005}{4}=0.001250 (B moves down, chord turns clockwise)
  • ψBC=−0.0056=−0.000833\psi_{BC}=-\dfrac{0.005}{6}=-0.000833 (C is higher than B, chord turns anticlockwise)
  • θA=0\theta_A=0, θC=+0.02\theta_C=+0.02 rad (clockwise)

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

  • AB (a=1a=1, b=3b=3): FEMAB=−4×1×3242=−2.250FEM_{AB}=-\dfrac{4\times1\times3^2}{4^2}=-2.250, FEMBA=+4×12×342=0.750FEM_{BA}=+\dfrac{4\times1^2\times3}{4^2}=0.750
  • BC: ∓2×6212=∓6.000\mp\dfrac{2\times6^2}{12}=\mp6.000

Step 3: Slope-deflection equations (numerical example, EI=20 000EI=20\,000 t m²)

  • MAB=10000.00(θB)−39.75M_{AB}=10000.00\left(\theta_{B}\right) - 39.75
  • MBA=10000.00(2θB)−36.75M_{BA}=10000.00\left(2\theta_{B}\right) - 36.75
  • MBC=13333.33(2θB+0.02000)+27.33M_{BC}=13333.33\left(2\theta_{B} + 0.02000\right) + 27.33
  • MCB=13333.33(0.04000+θB)+39.33M_{CB}=13333.33\left(0.04000 + \theta_{B}\right) + 39.33

Step 4: Equilibrium at B

MBA+MBC=0M_{BA}+M_{BC}=0 gives one equation in θB\theta_B:

[46666.6667]{θB}={−257.250}\begin{bmatrix}46666.6667\end{bmatrix}\begin{Bmatrix}\theta_{B}\end{Bmatrix}=\begin{Bmatrix}-257.250\end{Bmatrix} θB=−0.0055125\theta_{B}=-0.0055125

Step 5: End moments

EndLoads onlyMovements, per unit EITotal (EI = 20 000 t m²)
AB-1.125-0.004688-94.875
BA3.000-0.007500-147.000
BC-3.0000.007500147.000
CB7.5000.024583499.167

(For any EI: M=Mload+EI×(column 3)M=M_{load}+EI\times(\text{column 3}).)

Check: MBA+MBC=0.000M_{BA}+M_{BC}=0.000 ✓.

SFD and BMD (EI = 20 000 t m²)

MemberBM at first endBM at second endMax within member
AB-94.88147.00-
BC147.00-499.17-
Shears (t): AB: 63.47 at A, 59.47 after the 4 t load; BC: -101.69 at B falling at 2 t/m to -113.69 at C. Reactions: A: H=0.00H=0.00, V=63.47V=63.47, M=94.88M=94.88; B: H=0.00H=0.00, V=−161.16V=-161.16, M=0.00M=0.00; C: H=0.00H=0.00, V=113.69V=113.69, M=−499.17M=-499.17.

Answer: for EI=20 000EI=20\,000 t m²: MAB=−94.875M_{AB}=-94.875, MBA=−147.000M_{BA}=-147.000, MBC=147.000M_{BC}=147.000, MCB=499.167M_{CB}=499.167 tm; 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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