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Conjugate beam: slopes at supports, deflection at E

Short answer

Conjugate beam method with distributed M/EI load yields support slopes: 1636.67/EI rad clockwise at A, 1606.67/EI rad anticlockwise at B. Deflection at E (5 m from A) is 7281.25/EI kN·m³ downward.

Find slopes at supports and deflection at E of the beam given in figure below. Use conjugate beam method for deflection and slope calculations. [Figure: beam ABC; A hinge, B roller, span AB = 20 m with 5 kN/m UDL on AB; E is 5 m from A; overhang BC = 3 m with 3 kN at C; EI constant.]

Given data

Beam ABC: AB=20AB = 20 m (hinge at A, roller at B) with UDL 5 kN/m; overhang BC=3BC = 3 m with 3 kN at C. E is 5 m from A. EIEI constant.

Step 1: Reactions

RA=49.55R_{A} = 49.55 kN, RB=53.45R_{B} = 53.45 kN (positive = upward; check: ∑Fy=103.00\sum F_y = 103.00 kN equals the total load 103.00 kN).

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

Portion (m)MM (kNm)stiffnessArea of M/EIM/EIxˉ\bar x from A (m)
0 to 20−5x22+991x20- \frac{5 x^{2}}{2} + \frac{991 x}{20}EI3243.339.908
20 to 233x−693 x - 69EI-13.5021.000

(Stiffness is in terms of EIEI; "Area" is ∫M/EI dx\int M/EI\,dx in units of 1/EI1/EI; xˉ\bar x is the centroid distance from A.)

Step 3: Conjugate beam

The real beam has a hinge at A, a roller at the second support and a free end at the overhang tip, so the conjugate beam has a hinge at A, an internal hinge at the support and a fixed end at the tip. 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 beam about the support at x=20x = 20 m (conjugate moment is zero there):

RA′×20=(3243.33)(10.092)=32733.33R'_A\times20 = (3243.33)(10.092) = 32733.33 RA′=1636.667EI (slope at A, clockwise)R'_A = \frac{1636.667}{EI}\ \text{(slope at A, clockwise)}

At support A (x=0x = 0 m):

V′=RA′−∑A=1636.667−[0]=1636.667EI (slope, clockwise)V' = R'_A - \sum A = 1636.667 - [0] = \frac{1636.667}{EI}\ \text{(slope, clockwise)} M′=RA′ x−∑A(x−xˉ)=0.000−[0]=0.000EI (deflection, zero)M' = R'_A\,x - \sum A(x-\bar x) = 0.000 - [0] = \frac{0.000}{EI}\ \text{(deflection, zero)}

At E (5 m from A) (x=5x = 5 m):

V′=RA′−∑A=1636.667−[(515.21)]=1121.458EI (slope, clockwise)V' = R'_A - \sum A = 1636.667 - [(515.21)] = \frac{1121.458}{EI}\ \text{(slope, clockwise)} M′=RA′ x−∑A(x−xˉ)=8183.333−[(515.21)(1.751)]=7281.250EI (deflection, downward)M' = R'_A\,x - \sum A(x-\bar x) = 8183.333 - [(515.21)(1.751)] = \frac{7281.250}{EI}\ \text{(deflection, downward)}

At support B (x=20x = 20 m):

V′=RA′−∑A=1636.667−[(3243.33)]=−1606.667EI (slope, anticlockwise)V' = R'_A - \sum A = 1636.667 - [(3243.33)] = \frac{-1606.667}{EI}\ \text{(slope, anticlockwise)} M′=RA′ x−∑A(x−xˉ)=32733.333−[(3243.33)(10.092)]=0.000EI (deflection, zero)M' = R'_A\,x - \sum A(x-\bar x) = 32733.333 - [(3243.33)(10.092)] = \frac{0.000}{EI}\ \text{(deflection, zero)}

At C (free end) (x=23x = 23 m):

V′=RA′−∑A=1636.667−[(3243.33)+(−13.50)]=−1593.167EI (slope, anticlockwise)V' = R'_A - \sum A = 1636.667 - [(3243.33) + (-13.50)] = \frac{-1593.167}{EI}\ \text{(slope, anticlockwise)} M′=RA′ x−∑A(x−xˉ)=37643.333−[(3243.33)(13.092)+(−13.50)(2.000)]=−4793.000EI (deflection, upward)M' = R'_A\,x - \sum A(x-\bar x) = 37643.333 - [(3243.33)(13.092) + (-13.50)(2.000)] = \frac{-4793.000}{EI}\ \text{(deflection, upward)}

Answer: slope at A =1636.67EI= \dfrac{1636.67}{EI} (clockwise); slope at B =1606.67EI= \dfrac{1606.67}{EI} (anticlockwise); deflection at E =7281.25EI= \dfrac{7281.25}{EI} downward (kNm2^2/EI and kNm3^3/EI). (At C the deflection is 4793/EI4793/EI upward, which is not asked.)

✓ Answer checked by Claude Opus 5.5 (high effort)

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