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Conjugate beam: rotation at A, deflection at C

Short answer

Using conjugate beam, rotation at A is 210/EI rad clockwise; deflection at C is 180/EI upward. The conjugate beam had A simply supported, B internal hinge, C fixed, with M/(2EI) on AB and M/EI on BC.

Determine the rotation at A and deflection at C in the overhanging beam shown in fig-4 by using conjugate beam method. [Figure: beam ABC; A hinge, B roller; AB = 6 m (2I) and BC = 2 m (I); 60 kN/m UDL over the whole length.]

Data: AB=6AB = 6 m (2I2I), BC=2BC = 2 m (II) overhang, w=60w = 60 kN/m on the whole beam. Units: kN, m, EIEI taken for the section II.

Real beam: reactions and BM

RB×6=60×8×4⇒RB=320 kN,RA=480−320=160 kNMx=160x−30x2 (0≤x≤6),MB=−60×222=−120 kN m\begin{aligned} R_B\times 6 &= 60\times 8\times 4 \Rightarrow R_B = 320\ \text{kN}, \quad R_A = 480-320 = 160\ \text{kN}\\ M_x &= 160x - 30x^2 \ (0\le x\le 6), \quad M_B = -60\times\tfrac{2^2}{2} = -120\ \text{kN m} \end{aligned}

The loading on the conjugate beam is M/EIM/EI, so in ABAB it is M/(2EI)M/(2EI) and in BCBC it is M/EIM/EI.

Conjugate beam

Real hinge AA gives a simple support. Real roller BB (with overhang) gives an internal hinge. Real free end CC gives a fixed end.

 Real:   A o=======o B========= C (free)
 Conj.:  A o=======o hinge====== C (fixed)
         load = M/EI (sagging down, hogging up)

Span AB (simply supported at A, hinge at B)

Load q′=160x−30x22EI=80x−15x2EIq' = \dfrac{160x-30x^2}{2EI} = \dfrac{80x-15x^2}{EI}; total load =∫06q′ dx=360EI=\int_0^6 q'\,dx = \dfrac{360}{EI}.

Taking moments about the hinge BB (moment of conjugate beam is zero there):

RA′=16∫06(80x−15x2)(6−x) dx=12606EI=210EIR'_A = \frac{1}{6}\int_0^6 (80x-15x^2)(6-x)\,dx = \frac{1260}{6EI} = \frac{210}{EI} RB′=360−210EI=150EIR'_B = \frac{360-210}{EI} = \frac{150}{EI}

Span BC (cantilever, fixed at C)

M/EIM/EI in BCBC is negative (hogging), M=−30(2−x′)2M = -30(2-x')^2 with x′x' from BB. Its load is upward on the conjugate beam: total =∫0230(2−x′)2dx′=80/EI= \int_0^2 30(2-x')^2dx' = 80/EI, with moment about CC equal to ∫0230(2−x′)3dx′=120/EI\int_0^2 30(2-x')^3dx' = 120/EI.

The hinge BB passes the force 150/EI150/EI downward onto the cantilever. Moment at the fixed end CC:

MC′=150×2−120=180EI (hogging)M'_C = 150\times 2 - 120 = \frac{180}{EI}\ (\text{hogging})

Results

  • Rotation at AA = shear in conjugate beam at AA: θA=210EI\theta_A = \dfrac{210}{EI} (clockwise).
  • Deflection at CC = moment in conjugate beam at CC: yC=180EIy_C = \dfrac{180}{EI}, and since the conjugate moment is hogging it is upward.

Answer: θA=210/EI\theta_A = 210/EI kN m² (clockwise), yC=180/EIy_C = 180/EI kN m³ (upward).

✓ Answer checked by Claude Opus 5.5 (high effort)

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