Skip to main content

Slope deflection: three-span beam with settlement

Short answer

Use slope-deflection equations including support settlement chord rotations, with EI=800 kNm^2. Solve joint equilibrium for theta_B=-0.003295 and theta_C=0.0011275. Final moments: M_AB=-7.15, M_BA=3.98, M_BC=-3.98, M_CB=4.85, M_CD=-4.85, M_DC=4.78 kNm.

A three-spanned continuous beam is fixed at both extreme ends. The left span is of sectional stiffness EI and is loaded with a uniform distributed load of intensity 2 kN/m. The mid span is of stiffness 2 EI and has a vertical concentrated force of magnitude 5 kN applied at a point 2 m from the right end. The right span is of sectional stiffness EI and is centrally loaded with a vertical concentrated force of magnitude 8 kN. The left span is of length 6 m and the other two are of 5 m. The left middle support settles 2 mm down and right middle support is lifted 3 mm up. Analyse using the slope deflection method and draw bending moment diagram for the beam if all the forces being applied are directed vertically downward. Take EI=8×1011 N-mm2EI = 8\times10^{11}\ \text{N-mm}^2.

Data: three spans AB = 6 m (EIEI, 2 kN/m), BC = 5 m (2EI2EI, 5 kN at 2 m from C, i.e. 3 m from B), CD = 5 m (EIEI, 8 kN at mid-span); A and D are fixed. Support B settles 2 mm and support C is lifted 3 mm. EI=8×1011EI=8\times10^{11} N mm² =800=800 kNm². Units: kN, m.

Chord rotations (clockwise +)

  • ψAB=0.0026=0.000333\psi_{AB}=\dfrac{0.002}{6}=0.000333 (B goes down)
  • ψBC=−(0.003+0.002)5=−0.001000\psi_{BC}=\dfrac{-(0.003+0.002)}{5}=-0.001000 (C is 5 mm above B)
  • ψCD=0.0035=0.000600\psi_{CD}=\dfrac{0.003}{5}=0.000600 (D is 3 mm below C)

Fixed-end moments (kNm, clockwise +)

  • AB: ∓2×6212=∓6.000\mp\dfrac{2\times6^2}{12}=\mp6.000
  • BC (a=3a=3, b=2b=2): FEMBC=−5×3×2252=−2.400FEM_{BC}=-\dfrac{5\times3\times2^2}{5^2}=-2.400, FEMCB=+5×32×252=3.600FEM_{CB}=+\dfrac{5\times3^2\times2}{5^2}=3.600
  • CD: ∓8×58=∓5.000\mp\dfrac{8\times5}{8}=\mp5.000

Slope-deflection equations (θA=θD=0\theta_A=\theta_D=0)

  • MAB=266.67(θB)−6.27M_{AB}=266.67\left(\theta_{B}\right) - 6.27
  • MBA=266.67(2θB)+5.73M_{BA}=266.67\left(2\theta_{B}\right) + 5.73
  • MBC=640.00(2θB+θC)−0.48M_{BC}=640.00\left(2\theta_{B} + \theta_{C}\right) - 0.48
  • MCB=640.00(2θC+θB)+5.52M_{CB}=640.00\left(2\theta_{C} + \theta_{B}\right) + 5.52
  • MCD=320.00(2θC)−5.58M_{CD}=320.00\left(2\theta_{C}\right) - 5.58
  • MDC=320.00(θC)+4.42M_{DC}=320.00\left(\theta_{C}\right) + 4.42

Equilibrium and solution

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

[1813.3333640.0000640.00001920.0000]{θBθC}={−5.2530.056}\begin{bmatrix}1813.3333 & 640.0000 \\ 640.0000 & 1920.0000\end{bmatrix}\begin{Bmatrix}\theta_{B} \\ \theta_{C}\end{Bmatrix}=\begin{Bmatrix}-5.253 \\ 0.056\end{Bmatrix} θB=−0.003295,θC=0.0011275\theta_{B}=-0.003295,\quad \theta_{C}=0.0011275

Final end moments (kNm)

EndMM (kNm)EndMM (kNm)
AB-7.15BA3.98
BC-3.98CB4.85
CD-4.85DC4.78

Checks:

  • Joint B: (3.98) + (-3.98) = 0.00 kNm (applied clockwise moment 0.00) ✓
  • Joint C: (4.85) + (-4.85) = 0.00 kNm (applied clockwise moment 0.00) ✓

Bending moment diagram (sagging +, kNm)

MemberBM at first endBM at second endMax within member
AB-7.15-3.983.51 at 3.26 m
BC-3.98-4.851.50 at 3.00 m
CD-4.85-4.785.18 at 2.50 m
Under the 5 kN load: 1.50 kNm; under the 8 kN load: 5.18 kNm.

Reactions (kN, kNm; support moment M anticlockwise +): A: H=0.00H=0.00, V=6.53V=6.53, M=7.15M=7.15; B: H=0.00H=0.00, V=7.30V=7.30, M=0.00M=0.00; C: H=0.00H=0.00, V=7.19V=7.19, M=0.00M=0.00; D: H=0.00H=0.00, V=3.99V=3.99, M=−4.78M=-4.78.

Answer: MAB=−7.15M_{AB}=-7.15, MBA=3.98M_{BA}=3.98, MBC=−3.98M_{BC}=-3.98, MCB=4.85M_{CB}=4.85, MCD=−4.85M_{CD}=-4.85, MDC=4.78M_{DC}=4.78 kNm.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Theory of Structures II chapter 3 questions →