Skip to main content

Conjugate beam: stepped symmetric beam

Short answer

With EI = 4×10⁶ kN·m², the conjugate beam method gives slopes: θ_A = 1.125×10⁻⁵ rad clockwise, θ_B = 5.625×10⁻⁶ rad clockwise, θ_C = 5.625×10⁻⁶ rad anticlockwise, θ_D = 1.125×10⁻⁵ rad anticlockwise. Deflections: y_B = y_C = 0.0141 mm downward; y_A = y_D = 0.

A symmetrical beam ABCD is simply supported at its ends A and D over a span of 6 m. It is made up of three portions with different values of I, the length of the middle portion with the value of 2I is 3 m and the portion with the value of I is 1.5 m each. The beam carries two point loads of 20 kN at B and C. Find the slope and deflection at A, B, C and D using the conjugate beam method. Take E=200 kN/mm2E = 200\ \text{kN/mm}^2 and I=2×1010 mm4I = 2\times10^{10}\ \text{mm}^4. [Figure: AB = 2 m? (I), BC (2I), CD (I); loads 20 kN at B and C; AB = BC = CD = 2 m as dimensioned.]

Given data

Symmetrical beam ABCD, simply supported at A and D, span 6 m, in three portions: AB (1.5 m, II), BC (3 m, 2I2I), CD (1.5 m, II) as stated in the question (so B and C are 1.5 m from the ends). Loads 20 kN at B and at C. E=200E = 200 kN/mm2=2×108^2 = 2\times10^8 kN/m2^2, I=2×1010I = 2\times10^{10} mm4=0.02^4 = 0.02 m4^4, so EI=4,000,000EI = 4,000,000 kNm2^2.

        20 kN        20 kN
 A -----v------------v----- D
 ^ 1.5 m B   3 m (2I) C 1.5 m ^
    (I)                  (I)

Step 1: Reactions

RA=20.00R_{A} = 20.00 kN, RD=20.00R_{D} = 20.00 kN (positive = upward; check: ∑Fy=40.00\sum F_y = 40.00 kN equals the total load 40.00 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 1.520x20 xEI22.501.000
1.5 to 4.530302EI45.003.000
4.5 to 6120−20x120 - 20 xEI22.505.000

(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 conjugate of a simply supported beam is a simply supported beam of the same span. 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=6x = 6 m (conjugate moment is zero there):

RA′×6=(22.50)(5.000)+(45.00)(3.000)+(22.50)(1.000)=270.00R'_A\times6 = (22.50)(5.000) + (45.00)(3.000) + (22.50)(1.000) = 270.00 RA′=45.000EI (slope at A, clockwise)R'_A = \frac{45.000}{EI}\ \text{(slope at A, clockwise)}

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

V′=RA′−∑A=45.000−[0]=45.000EI (slope, clockwise)V' = R'_A - \sum A = 45.000 - [0] = \frac{45.000}{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 B (x=1.5x = 1.5 m):

V′=RA′−∑A=45.000−[(22.50)]=22.500EI (slope, clockwise)V' = R'_A - \sum A = 45.000 - [(22.50)] = \frac{22.500}{EI}\ \text{(slope, clockwise)} M′=RA′ x−∑A(x−xˉ)=67.500−[(22.50)(0.500)]=56.250EI (deflection, downward)M' = R'_A\,x - \sum A(x-\bar x) = 67.500 - [(22.50)(0.500)] = \frac{56.250}{EI}\ \text{(deflection, downward)}

At C (x=4.5x = 4.5 m):

V′=RA′−∑A=45.000−[(22.50)+(45.00)]=−22.500EI (slope, anticlockwise)V' = R'_A - \sum A = 45.000 - [(22.50) + (45.00)] = \frac{-22.500}{EI}\ \text{(slope, anticlockwise)} M′=RA′ x−∑A(x−xˉ)=202.500−[(22.50)(3.500)+(45.00)(1.500)]=56.250EI (deflection, downward)M' = R'_A\,x - \sum A(x-\bar x) = 202.500 - [(22.50)(3.500) + (45.00)(1.500)] = \frac{56.250}{EI}\ \text{(deflection, downward)}

At D (x=6x = 6 m):

V′=RA′−∑A=45.000−[(22.50)+(45.00)+(22.50)]=−45.000EI (slope, anticlockwise)V' = R'_A - \sum A = 45.000 - [(22.50) + (45.00) + (22.50)] = \frac{-45.000}{EI}\ \text{(slope, anticlockwise)} M′=RA′ x−∑A(x−xˉ)=270.000−[(22.50)(5.000)+(45.00)(3.000)+(22.50)(1.000)]=0.000EI (deflection, zero)M' = R'_A\,x - \sum A(x-\bar x) = 270.000 - [(22.50)(5.000) + (45.00)(3.000) + (22.50)(1.000)] = \frac{0.000}{EI}\ \text{(deflection, zero)}

Results (symmetry check)

By symmetry θD=−θA\theta_D = -\theta_A and yC=yBy_C = y_B. With EI=4,000,000EI = 4,000,000 kNm2^2:

PointSlope (rad)Deflection (mm, downward)
A1.125×10−51.125\times10^{-5}0.0000
B5.625×10−65.625\times10^{-6}0.0141
C5.625×10−65.625\times10^{-6}0.0141
D1.125×10−51.125\times10^{-5}0.0000

Slopes: A is clockwise, B is clockwise, C is anticlockwise, D is anticlockwise.

Answer: θA=θD=45EI=1.125×10−5\theta_A = \theta_D = \dfrac{45}{EI} = 1.125\times10^{-5} rad, θB=θC=22.5EI=5.625×10−6\theta_B = \theta_C = \dfrac{22.5}{EI} = 5.625\times10^{-6} rad (opposite senses), and yB=yC=56.25EI=0.0141y_B = y_C = \dfrac{56.25}{EI} = 0.0141 mm downward; yA=yD=0y_A = y_D = 0.

If the figure's dimensions are used instead (AB = BC = CD = 2 m, with II, 2I2I, II): θA=60EI=1.500×10−5\theta_A = \dfrac{60}{EI} = 1.500\times10^{-5} rad, θB=20EI=5.000×10−6\theta_B = \dfrac{20}{EI} = 5.000\times10^{-6} rad, yB=yC=93.33EI=0.0233y_B = y_C = \dfrac{93.33}{EI} = 0.0233 mm.

✓ Answer checked by Claude Opus 5.5 (high effort)

All Theory of Structures I chapter 4 questions →