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Moment area: B, C, maximum deflection

Short answer

Moment area method: deflection at B = 5550/EI downward, at C = 4300/EI downward. Maximum deflection occurs where slope zero between B and C, at 5.08 m from A, magnitude = 6852/EI downward. Analysis uses tangent at A, M/EI area moments, and condition for zero slope.

Calculate deflection at points B and C of the given simply supported beam using moment area method. Also calculate the location and magnitude of maximum deflection. Take EI to be constant. [Figure: beam ABCD, A hinge, D roller; AB = 3 m with 200 kN at B; BC = 5 m with 300 kN at C; CD = 2 m.]

Given data

Simply supported beam ABCD, span AD=10AD = 10 m: A hinge, D roller, AB=3AB = 3 m (200 kN at B), BC=5BC = 5 m (300 kN at C), CD=2CD = 2 m. EIEI constant. xx is measured from A.

       200 kN         300 kN
 A ------v--------------v----- D
 ^  3 m  B     5 m      C 2 m  ^

Step 1: Reactions

RA=200.00R_{A} = 200.00 kN, RD=300.00R_{D} = 300.00 kN (positive = upward; check: ∑Fy=500.00\sum F_y = 500.00 kN equals the total load 500.00 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 3200x200 xEI900.002.000
3 to 8600600EI3000.005.500
8 to 103000−300x3000 - 300 xEI600.008.667

(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: Tangent at A

Deviation of the support at x=10x = 10 m from the tangent at A (Theorem II, moment of the M/EIM/EI area about that support):

t=(900.00)(8.000)+(3000.00)(4.500)+(600.00)(1.333)=21500.00EIt = (900.00)(8.000) + (3000.00)(4.500) + (600.00)(1.333) = \frac{21500.00}{EI}

That support does not deflect, so θA=−t/10\theta_A = -t/10:

θA=−2150.000EI (clockwise)\theta_A = \frac{-2150.000}{EI}\ \text{(clockwise)}

At B (x=3x = 3 m):

θ=θA+∑A=−2150.000+[(900.00)]=−1250.000EI (clockwise)\theta = \theta_A + \sum A = -2150.000 + [(900.00)] = \frac{-1250.000}{EI}\ \text{(clockwise)} y=θA x+tP/A=−6450.000+[(900.00)(1.000)]=−5550.000EI (downward)y = \theta_A\,x + t_{P/A} = -6450.000 + [(900.00)(1.000)] = \frac{-5550.000}{EI}\ \text{(downward)}

At C (x=8x = 8 m):

θ=θA+∑A=−2150.000+[(900.00)+(3000.00)]=1750.000EI (anticlockwise)\theta = \theta_A + \sum A = -2150.000 + [(900.00) + (3000.00)] = \frac{1750.000}{EI}\ \text{(anticlockwise)} y=θA x+tP/A=−17200.000+[(900.00)(6.000)+(3000.00)(2.500)]=−4300.000EI (downward)y = \theta_A\,x + t_{P/A} = -17200.000 + [(900.00)(6.000) + (3000.00)(2.500)] = \frac{-4300.000}{EI}\ \text{(downward)}

At the point of maximum deflection (x=5.08333x = 5.08333 m):

θ=θA+∑A=−2150.000+[(900.00)+(1250.00)]=0.000EI (zero)\theta = \theta_A + \sum A = -2150.000 + [(900.00) + (1250.00)] = \frac{0.000}{EI}\ \text{(zero)} y=θA x+tP/A=−10929.167+[(900.00)(3.083)+(1250.00)(1.042)]=−6852.083EI (downward)y = \theta_A\,x + t_{P/A} = -10929.167 + [(900.00)(3.083) + (1250.00)(1.042)] = \frac{-6852.083}{EI}\ \text{(downward)}

Maximum deflection

The deflection is maximum where the slope is zero. The slope at B is −1250/EI-1250/EI (clockwise) and at C it is +1750/EI+1750/EI, so the zero lies between B and C. In BC, M/EI=600/EIM/EI = 600/EI is constant, so the slope changes by 600/EI600/EI per metre:

−1250+600 (x−3)=0  ⇒  x=3+2.083=5.083 m from A-1250 + 600\,(x - 3) = 0 \;\Rightarrow\; x = 3 + 2.083 = 5.083\ \text{m from A}

The deflection there (Step 3 tangent offset, from the same formula) is

ymax=θAx+tP/A=−6852.08EIy_{max} = \theta_A x + t_{P/A} = \frac{-6852.08}{EI}

Answer: deflection at B =5550/EI= 5550/EI downward; at C =4300/EI= 4300/EI downward (kNm3^3/EI). Maximum deflection =6852.1/EI= 6852.1/EI downward at 5.0835.083 m from A (and 4.917 m from D).

✓ Answer checked by Claude Opus 5.5 (high effort)

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