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Conjugate beam: deflection at B and D

Short answer

Reactions: 3 kN at A, 41 kN at C. The conjugate beam with stiffness 2EI on AC and EI on CB gives deflection at D (under 20 kN) = 20.625/EI downward and at free end B = 103.125/EI downward, where EI is the reference flexural rigidity.

Calculate deflection at point B and D using conjugate beam method. [Figure: beam ABCD; A hinge, C roller; AC with 2EI, AD = 5 m with a 20 kN load at D, DC = 3 m; overhang CB = 3 m with EI carrying 8 kN/m UDL.]

Given data

Beam ABCD as labelled: A hinge at 0, D at 5 m (20 kN down), C roller at 8 m (DC=3DC = 3 m), overhang CB=3CB = 3 m with UDL 8 kN/m and free end B at 11 m. ACAC has 2EI2EI and the overhang CBCB has EIEI. Required: deflection at B (free end) and D.

        20 kN                 8 kN/m (EI)
 A -------v---------- C =============== B
 ^   5 m  D   3 m (2EI) ^      3 m

Step 1: Reactions

RA=3.00R_{A} = 3.00 kN, RC=41.00R_{C} = 41.00 kN (positive = upward; check: ∑Fy=44.00\sum F_y = 44.00 kN equals the total load 44.00 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 53x3 x2EI18.753.333
5 to 8100−17x100 - 17 x2EI-15.757.714
8 to 11−4x2+88x−484- 4 x^{2} + 88 x - 484EI-36.008.750

(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=8x = 8 m (conjugate moment is zero there):

RA′×8=(18.75)(4.667)+(−15.75)(0.286)=83.00R'_A\times8 = (18.75)(4.667) + (-15.75)(0.286) = 83.00 RA′=10.375EI (slope at A, clockwise)R'_A = \frac{10.375}{EI}\ \text{(slope at A, clockwise)}

At D (20 kN) (x=5x = 5 m):

V′=RA′−∑A=10.375−[(18.75)]=−8.375EI (slope, anticlockwise)V' = R'_A - \sum A = 10.375 - [(18.75)] = \frac{-8.375}{EI}\ \text{(slope, anticlockwise)} M′=RA′ x−∑A(x−xˉ)=51.875−[(18.75)(1.667)]=20.625EI (deflection, downward)M' = R'_A\,x - \sum A(x-\bar x) = 51.875 - [(18.75)(1.667)] = \frac{20.625}{EI}\ \text{(deflection, downward)}

At B (free end) (x=11x = 11 m):

V′=RA′−∑A=10.375−[(18.75)+(−15.75)+(−36.00)]=43.375EI (slope, clockwise)V' = R'_A - \sum A = 10.375 - [(18.75) + (-15.75) + (-36.00)] = \frac{43.375}{EI}\ \text{(slope, clockwise)} M′=RA′ x−∑A(x−xˉ)=114.125−[(18.75)(7.667)+(−15.75)(3.286)+(−36.00)(2.250)]=103.125EI (deflection, downward)M' = R'_A\,x - \sum A(x-\bar x) = 114.125 - [(18.75)(7.667) + (-15.75)(3.286) + (-36.00)(2.250)] = \frac{103.125}{EI}\ \text{(deflection, downward)}

Answer: deflection at D =20.625EI= \dfrac{20.625}{EI} downward; deflection at the free end B =103.125EI= \dfrac{103.125}{EI} downward (kNm3^3/EI).

✓ Answer checked by Claude Opus 5.5 (high effort)

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