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Conjugate beam: slope and deflection at free end C

Short answer

Conjugate beam loaded with the M/EI diagram gives at free end C: slope 46/EI rad anticlockwise and deflection 190.67/EI kN·m³ upward.

Using conjugate beam method, calculate slope and deflection at point C, free end of the beam, loaded as shown below. EI is constant. [Figure: beam ABC; A hinge, B roller 8 m from A; 2 kN/m UDL over AB; 10 kN at D, 4 m from A; overhang BC = 4 m with 5 kN at 2 m from B.]

Given data

Beam ABC: A hinge at 0, B roller at 8 m. UDL 2 kN/m over AB; 10 kN at D (4 m from A); overhang BC=4BC = 4 m with 5 kN at 2 m from B (at 10 m from A). C is the free end at 12 m. EIEI constant.

        10 kN   2 kN/m          5 kN
 A ------v============ B ------v------- C
 ^  4 m  D     4 m     ^  2 m     2 m

Step 1: Reactions

RA=11.75R_{A} = 11.75 kN, RB=19.25R_{B} = 19.25 kN (positive = upward; check: ∑Fy=31.00\sum F_y = 31.00 kN equals the total load 31.00 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 4−x2+47x4- x^{2} + \frac{47 x}{4}EI72.672.569
4 to 8−x2+7x4+40- x^{2} + \frac{7 x}{4} + 40EI52.674.962
8 to 105x−505 x - 50EI-10.008.667
10 to 1200EI0.00-

(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=(72.67)(5.431)+(52.67)(3.038)=554.67R'_A\times8 = (72.67)(5.431) + (52.67)(3.038) = 554.67 RA′=69.333EI (slope at A, clockwise)R'_A = \frac{69.333}{EI}\ \text{(slope at A, clockwise)}

At D (10 kN) (x=4x = 4 m):

V′=RA′−∑A=69.333−[(72.67)]=−3.333EI (slope, anticlockwise)V' = R'_A - \sum A = 69.333 - [(72.67)] = \frac{-3.333}{EI}\ \text{(slope, anticlockwise)} M′=RA′ x−∑A(x−xˉ)=277.333−[(72.67)(1.431)]=173.333EI (deflection, downward)M' = R'_A\,x - \sum A(x-\bar x) = 277.333 - [(72.67)(1.431)] = \frac{173.333}{EI}\ \text{(deflection, downward)}

At C (free end) (x=12x = 12 m):

V′=RA′−∑A=69.333−[(72.67)+(52.67)+(−10.00)]=−46.000EI (slope, anticlockwise)V' = R'_A - \sum A = 69.333 - [(72.67) + (52.67) + (-10.00)] = \frac{-46.000}{EI}\ \text{(slope, anticlockwise)} M′=RA′ x−∑A(x−xˉ)=832.000−[(72.67)(9.431)+(52.67)(7.038)+(−10.00)(3.333)]=−190.667EI (deflection, upward)M' = R'_A\,x - \sum A(x-\bar x) = 832.000 - [(72.67)(9.431) + (52.67)(7.038) + (-10.00)(3.333)] = \frac{-190.667}{EI}\ \text{(deflection, upward)}

Answer: slope at C =46EI= \dfrac{46}{EI} (anticlockwise); deflection at C =190.67EI= \dfrac{190.67}{EI} upward (kNm2^2/EI and kNm3^3/EI). (The deflection under the 10 kN load at D is 173.33/EI173.33/EI downward.)

✓ Answer checked by Claude Opus 5.5 (high effort)

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