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Deflection at B, C and slope at A, D

Short answer

Downward deflection at B: 6.66/EI m, at C: 9.65/EI m. Slope at A: 7.41/EI rad clockwise; at D: 4.34/EI rad anticlockwise (EI in kN·m²).

Determine deflection at points B and C and slope at points A and D. [Figure: beam A-B-C-D-E with EI constant; hinge support at A and roller support at D; 5 kN point load at B; 1 kN/m UDL over C to D (3 m); 2 kNm couple at the overhanging end E; lengths A-B 1 m, B-C 1 m, C-D 3 m, D-E 2 m.]

Reading of the figure: AB=1AB = 1 m, BC=1BC = 1 m, CD=3CD = 3 m, DE=2DE = 2 m; hinge at A (x = 0) and roller at D (x = 5 m). Loads: 5 kN at B (x = 1), UDL 1 kN/m over CD (x = 2 to 5), and a 2 kN·m couple at the free end E (taken clockwise). EIEI is constant. Deflection is taken positive upward.

Reactions

Moments about A (anticlockwise positive):

RD(5)−5(1)−3(3.5)−2=0⇒RD=3.5 kN,RA=5+3−3.5=4.5 kNR_D(5) - 5(1) - 3(3.5) - 2 = 0 \Rightarrow R_D = 3.5\ \text{kN}, \qquad R_A = 5 + 3 - 3.5 = 4.5\ \text{kN}

Macaulay's method

The UDL ends at D, so it is continued to the end and cancelled by an equal upward load (+1 kN/m beyond D). Bending moment (sagging positive) at a section xx from A:

EId2ydx2=4.5x−5⟨x−1⟩−12⟨x−2⟩2+3.5⟨x−5⟩+12⟨x−5⟩2+2⟨x−7⟩0EI\frac{d^2y}{dx^2} = 4.5x - 5\langle x-1\rangle - \frac{1}{2}\langle x-2\rangle^2 + 3.5\langle x-5\rangle + \frac{1}{2}\langle x-5\rangle^2 + 2\langle x-7\rangle^0

Integrating:

EI θ=2.25x2−2.5⟨x−1⟩2−16⟨x−2⟩3+1.75⟨x−5⟩2+16⟨x−5⟩3+2⟨x−7⟩+C1EI\,\theta = 2.25x^2 - 2.5\langle x-1\rangle^2 - \frac{1}{6}\langle x-2\rangle^3 + 1.75\langle x-5\rangle^2 + \frac{1}{6}\langle x-5\rangle^3 + 2\langle x-7\rangle + C_1 EI y=0.75x3−56⟨x−1⟩3−124⟨x−2⟩4+712⟨x−5⟩3+124⟨x−5⟩4+⟨x−7⟩2+C1x+C2EI\,y = 0.75x^3 - \frac{5}{6}\langle x-1\rangle^3 - \frac{1}{24}\langle x-2\rangle^4 + \frac{7}{12}\langle x-5\rangle^3 + \frac{1}{24}\langle x-5\rangle^4 + \langle x-7\rangle^2 + C_1x + C_2

Constants

  • At A, y=0y = 0 at x=0x = 0: C2=0C_2 = 0.
  • At D, y=0y = 0 at x=5x = 5: 0.75(125)−56(64)−124(81)+5C1=0⇒C1=−7.40830.75(125) - \frac{5}{6}(64) - \frac{1}{24}(81) + 5C_1 = 0 \Rightarrow C_1 = -7.4083

Slopes at A and D

EI θA=C1=−7.408 kN⋅m2⇒θA=7.408EI rad (clockwise)EI\,\theta_A = C_1 = -7.408\ \text{kN·m}^2 \quad\Rightarrow\quad \theta_A = \frac{7.408}{EI}\ \text{rad (clockwise)} EI θD=2.25(25)−2.5(16)−276+C1=4.342 kN⋅m2⇒θD=4.342EI rad (anticlockwise)EI\,\theta_D = 2.25(25) - 2.5(16) - \frac{27}{6} + C_1 = 4.342\ \text{kN·m}^2 \quad\Rightarrow\quad \theta_D = \frac{4.342}{EI}\ \text{rad (anticlockwise)}

Deflections at B and C

EI yB=0.75(1)+C1(1)=−6.658 kN⋅m3⇒yB=6.658EI downwardEI\,y_B = 0.75(1) + C_1(1) = -6.658\ \text{kN·m}^3 \Rightarrow y_B = \frac{6.658}{EI}\ \text{downward} EI yC=0.75(8)−56(1)+C1(2)=−9.650 kN⋅m3⇒yC=9.650EI downwardEI\,y_C = 0.75(8) - \frac{5}{6}(1) + C_1(2) = -9.650\ \text{kN·m}^3 \Rightarrow y_C = \frac{9.650}{EI}\ \text{downward}

Answer (with EIEI in kN·m²): yB=6.66/EIy_B = 6.66/EI and yC=9.65/EIy_C = 9.65/EI (downward); θA=7.41/EI\theta_A = 7.41/EI (clockwise) and θD=4.34/EI\theta_D = 4.34/EI (anticlockwise).

✓ Answer checked by Claude Opus 5.5 (high effort)

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