Skip to main content

Slope deflection: beam with 50 kN and 30 kN

Short answer

Slope-deflection method: solving for rotations, the end moments are M_AB = -23.63, M_BA = 17.18, M_BC = -17.18, M_CB = 17.75, M_CD = -17.75, M_DC = 0 kNm; sagging moments under concentrated loads are 27.27 kNm and 21.13 kNm respectively.

Analyse the beam loaded as shown in the figure below by the slope deflection method. Also draw the bending moment diagram (BMD). [Figure: beam ABCD, A fixed; AB = 2.5 m + 1.5 m (3EI) with 50 kN at 2.5 m from A; BC = 4 m (2EI) with 10 kN/m UDL; CD = 2 m + 2 m (1.5EI) with 30 kN at mid-span; D roller.]

Data: A fixed; AB = 2.5 m + 1.5 m = 4 m (3EI) with 50 kN at 2.5 m from A; BC = 4 m (2EI) with 10 kN/m; CD = 2 m + 2 m = 4 m (1.5EI) with 30 kN at mid-span; D is a roller; B and C simple supports. No settlement.

Fixed-end moments (clockwise +)

  • AB (a=2.5a=2.5, b=1.5b=1.5): FEMAB=−50×2.5×1.5242=−17.58FEM_{AB}=-\dfrac{50\times2.5\times1.5^2}{4^2}=-17.58, FEMBA=+50×2.52×1.542=29.30FEM_{BA}=+\dfrac{50\times2.5^2\times1.5}{4^2}=29.30 kNm
  • BC: ∓10×4212=∓13.33\mp\dfrac{10\times4^2}{12}=\mp13.33 kNm
  • CD: ∓30×48=∓15\mp\dfrac{30\times4}{8}=\mp15 kNm

Slope-deflection equations

  • MAB=2(3EI)4(θB)−17.58M_{AB}=\frac{2(3EI)}{4}\left(\theta_{B}\right) - 17.58
  • MBA=2(3EI)4(2θB)+29.30M_{BA}=\frac{2(3EI)}{4}\left(2\theta_{B}\right) + 29.30
  • MBC=2(2EI)4(2θB+θC)−13.33M_{BC}=\frac{2(2EI)}{4}\left(2\theta_{B} + \theta_{C}\right) - 13.33
  • MCB=2(2EI)4(2θC+θB)+13.33M_{CB}=\frac{2(2EI)}{4}\left(2\theta_{C} + \theta_{B}\right) + 13.33
  • MCD=2(1.5EI)4(2θC+θD)−15.00M_{CD}=\frac{2(1.5EI)}{4}\left(2\theta_{C} + \theta_{D}\right) - 15.00
  • MDC=2(1.5EI)4(2θD+θC)+15.00M_{DC}=\frac{2(1.5EI)}{4}\left(2\theta_{D} + \theta_{C}\right) + 15.00

Equilibrium

  • Joint B: MBA+MBC=0M_{BA}+M_{BC}=0 Joint C: MCB+MCD=0M_{CB}+M_{CD}=0 Roller D: MDC=0M_{DC}=0
EI[5.00001.00000.00001.00003.50000.75000.00000.75001.5000]{θBθCθD}={−15.9641.667−15.000}EI\begin{bmatrix}5.0000 & 1.0000 & 0.0000 \\ 1.0000 & 3.5000 & 0.7500 \\ 0.0000 & 0.7500 & 1.5000\end{bmatrix}\begin{Bmatrix}\theta_{B} \\ \theta_{C} \\ \theta_{D}\end{Bmatrix}=\begin{Bmatrix}-15.964 \\ 1.667 \\ -15.000\end{Bmatrix} EIθB=−4.0378,EIθC=4.2254,EIθD=−12.1127EI\theta_{B}=-4.0378,\quad EI\theta_{C}=4.2254,\quad EI\theta_{D}=-12.1127

Final end moments (kNm)

EndMM (kNm)EndMM (kNm)
AB-23.63BA17.18
BC-17.18CB17.75
CD-17.75DC0.00

Checks:

  • Joint B: (17.18) + (-17.18) = 0.00 kNm (applied clockwise moment 0.00) ✓
  • Joint C: (17.75) + (-17.75) = 0.00 kNm (applied clockwise moment 0.00) ✓
  • Joint D: (0.00) = 0.00 kNm (applied clockwise moment 0.00) ✓

Bending moment diagram ordinates (sagging +, kNm)

MemberBM at first endBM at second endMax within member
AB-23.63-17.1827.27 at 2.50 m
BC-17.18-17.752.54 at 1.99 m
CD-17.750.0021.13 at 2.00 m

Reactions: A: H=0.00H=0.00, V=20.36V=20.36, M=23.63M=23.63; B: H=0.00H=0.00, V=49.50V=49.50, M=0.00M=0.00; C: H=0.00H=0.00, V=39.58V=39.58, M=0.00M=0.00; D: H=0.00H=0.00, V=10.56V=10.56, M=0.00M=0.00.

Answer: MAB=−23.63M_{AB}=-23.63, MBA=17.18M_{BA}=17.18, MBC=−17.18M_{BC}=-17.18, MCB=17.75M_{CB}=17.75, MCD=−17.75M_{CD}=-17.75, MDC=0M_{DC}=0 kNm; BM at the load points: 27.27 kNm under 50 kN, 21.13 kNm under 30 kN.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Theory of Structures II chapter 3 questions →