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Conjugate beam: vertical deflection and rotation at C

Short answer

Conjugate beam analysis with M/EI as load gives free end response. The deflection at C is 41.25/EI kN·m³ downward and the rotation is 27.29/EI rad clockwise.

Determine the vertical deflection and rotation at free end C of the overhanging beam ABC loaded as shown in figure below by using conjugate beam method. [Figure: beam ABC; AB = 5 m with 5 kN/m UDL; overhang BC = 2 m with 10 kN at C.]

Given data

Overhanging beam ABC: AB=5AB = 5 m with UDL 5 kN/m, overhang BC=2BC = 2 m with 10 kN at C. EIEI constant.

Step 1: Reactions

RA=8.50R_{A} = 8.50 kN, RB=26.50R_{B} = 26.50 kN (positive = upward; check: ∑Fy=35.00\sum F_y = 35.00 kN equals the total load 35.00 kN).

Step 2: Bending moment diagram (sagging +), as M/EIM/EI pieces

In AB, M=8.5x−2.5x2M = 8.5x - 2.5x^2. This is the free (simply supported) parabola of the UDL plus a hogging triangle caused by the overhang moment MB=−10×2=−20M_B = -10\times2 = -20 kNm. In BC, M=10x−70M = 10x - 70.

PieceArea of M/EIM/EIxˉ\bar x from A (m)
Parabola on AB (peak wL2/8=15.625wL^2/8 = 15.625 kNm)23(5)(15.625)=+52.083\tfrac23(5)(15.625) = +52.0832.500
Triangle on AB (0 at A to −20-20 at B)12(5)(−20)=−50.000\tfrac12(5)(-20) = -50.0003.333
Triangle on BC (−20-20 at B to 0 at C)12(2)(−20)=−20.000\tfrac12(2)(-20) = -20.0005.667

(Areas are in units of 1/EI1/EI; the net area on AB is +2.083+2.083.)

Step 3: Conjugate beam

The real beam has a hinge at A, a roller at B and a free end at C, so the conjugate beam has a simple support at A, an internal hinge at B and a fixed end at C. It carries the M/EIM/EI diagram of Step 2 as load (sagging M/EIM/EI acts downward, hogging acts upward). Conjugate shear V′V' = slope (positive = clockwise) and conjugate moment M′M' = deflection (positive = downward).

Step 4: Conjugate reaction at A (slope at A)

Taking moments of the conjugate span AB about the hinge B (conjugate moment is zero there):

RA′×5=(52.083)(2.500)+(−50.000)(1.667)=130.208−83.333=46.875R'_A\times5 = (52.083)(2.500) + (-50.000)(1.667) = 130.208 - 83.333 = 46.875 RA′=9.375EI (slope at A, clockwise)R'_A = \frac{9.375}{EI}\ \text{(slope at A, clockwise)}

At C (free end) (x=7x = 7 m):

V′=RA′−∑A=9.375−[(52.083)+(−50.000)+(−20.000)]=27.292EI (slope, clockwise)V' = R'_A - \sum A = 9.375 - [(52.083) + (-50.000) + (-20.000)] = \frac{27.292}{EI}\ \text{(slope, clockwise)} M′=RA′ x−∑A(x−xˉ)=65.625−[(52.083)(4.500)+(−50.000)(3.667)+(−20.000)(1.333)]=65.625−24.375=41.250EI (deflection, downward)M' = R'_A\,x - \sum A(x-\bar x) = 65.625 - [(52.083)(4.500) + (-50.000)(3.667) + (-20.000)(1.333)] = 65.625 - 24.375 = \frac{41.250}{EI}\ \text{(deflection, downward)}

Answer: deflection at the free end C =41.25EI= \dfrac{41.25}{EI} downward; rotation at C =27.29EI= \dfrac{27.29}{EI} rad (clockwise) (kNm3^3/EI and kNm2^2/EI).

✓ Answer checked by Claude Opus 5.5 (high effort)

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