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Moment area: slope and deflection under 50 kN

Short answer

Using the moment-area method: θA = 355.56/EI clockwise, θB = 444.44/EI anticlockwise. Deflection at C is 1244.4/EI, at D is 1422.2/EI, both downward. Maximum deflection is 1548.3/EI downward at 6.532 m from A.

Using moment area method, calculate the slope at supports, deflection at points C and D. Also calculate maximum deflection in the beam and its location. [Figure: simply supported beam AB with C and D; AC = CD = DB = 4 m (span 12 m); 50 kN at D; EI constant.]

Given data

Simply supported beam AB, L=12L = 12 m. AC=CD=DB=4AC = CD = DB = 4 m. 50 kN at D (8 m from A). EIEI constant.

                       50 kN
 A ------- C ------- D v ----- B
 ^   4 m     4 m         4 m   ^

Step 1: Reactions

RA=16.67R_{A} = 16.67 kN, RB=33.33R_{B} = 33.33 kN (positive = upward; check: ∑Fy=50.00\sum F_y = 50.00 kN equals the total load 50.00 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 850x3\frac{50 x}{3}EI533.335.333
8 to 12400−100x3400 - \frac{100 x}{3}EI266.679.333

(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=12x = 12 m from the tangent at A (Theorem II, moment of the M/EIM/EI area about that support):

t=(533.33)(6.667)+(266.67)(2.667)=4266.67EIt = (533.33)(6.667) + (266.67)(2.667) = \frac{4266.67}{EI}

That support does not deflect, so θA=−t/12\theta_A = -t/12:

θA=−355.556EI (clockwise)\theta_A = \frac{-355.556}{EI}\ \text{(clockwise)}

At C (x=4x = 4 m):

θ=θA+∑A=−355.556+[(133.33)]=−222.222EI (clockwise)\theta = \theta_A + \sum A = -355.556 + [(133.33)] = \frac{-222.222}{EI}\ \text{(clockwise)} y=θA x+tP/A=−1422.222+[(133.33)(1.333)]=−1244.444EI (downward)y = \theta_A\,x + t_{P/A} = -1422.222 + [(133.33)(1.333)] = \frac{-1244.444}{EI}\ \text{(downward)}

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

θ=θA+∑A=−355.556+[(533.33)]=177.778EI (anticlockwise)\theta = \theta_A + \sum A = -355.556 + [(533.33)] = \frac{177.778}{EI}\ \text{(anticlockwise)} y=θA x+tP/A=−2844.444+[(533.33)(2.667)]=−1422.222EI (downward)y = \theta_A\,x + t_{P/A} = -2844.444 + [(533.33)(2.667)] = \frac{-1422.222}{EI}\ \text{(downward)}

At the point of maximum deflection (x=6.532x = 6.532 m):

θ=θA+∑A=−355.556+[(355.56)]=0 (zero slope)\theta = \theta_A + \sum A = -355.556 + [(355.56)] = 0\ \text{(zero slope)} y=θA x+tP/A=−2322.489+[(355.56)(2.177)]=−1548.319EI (downward)y = \theta_A\,x + t_{P/A} = -2322.489 + [(355.56)(2.177)] = \frac{-1548.319}{EI}\ \text{(downward)}

Slope at the supports

θA=355.56/EI\theta_A = 355.56/EI (clockwise), as found above. At B (x=12x = 12 m): θB=θA+total area=−355.56+800=444.44\theta_B = \theta_A + \text{total area} = -355.56 + 800 = 444.44, so θB=444.44EI\theta_B = \dfrac{444.44}{EI} (anticlockwise). (Total area of the M/EIM/EI triangle =12×12×133.33=800= \tfrac12\times12\times133.33 = 800.)

Maximum deflection

The slope is zero in the portion AD, where M=16.667xM = 16.667x. Slope: θ(x)=−355.56+8.333x2\theta(x) = -355.56 + 8.333x^2. Setting it to zero:

x=355.568.333=6.532 m from Ax = \sqrt{\frac{355.56}{8.333}} = 6.532\ \text{m from A}

This lies in AD, so the assumption is valid. The deflection there, from the same formula, is ymax=1548.3EIy_{max} = \dfrac{1548.3}{EI} downward.

Answer: θA=355.56/EI\theta_A = 355.56/EI (clockwise), θB=444.44/EI\theta_B = 444.44/EI (anticlockwise); deflection at C =1244.4/EI= 1244.4/EI, at D =1422.2/EI= 1422.2/EI (both downward); maximum deflection =1548.3/EI= 1548.3/EI downward at 6.5326.532 m from A.

✓ Answer checked by Claude Opus 5.5 (high effort)

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