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Conjugate beam: slope and deflection at free end

Short answer

By conjugate beam method, real free end C becomes fixed, interior support B becomes internal hinge. M/EI areas with variable EI (EI for AB, 2EI for BC) give shear and moment. Slope at C = 160/EI clockwise; deflection at C = 586.7/EI downward (rad and m for EI in kNm^2).

Determine the slope and deflections at the free end of the beam shown in figure below using conjugate beam method. [Figure: beam ABC; A hinge; D at 4 m from A carries a 24 kN downward load; B is a support 2 m from D; the portion A to B has EI; overhang BC of 4 m has 2EI and carries a 10 kN/m UDL.]

Given data

Beam ABC: A hinge at the left end, D at 4 m from A (24 kN down), B roller support at 6 m from A, overhang BC = 4 m (stiffness 2EI2EI) with UDL 10 kN/m. Portion AB has EIEI. Required: slope and deflection at the free end C.

        24 kN                    10 kN/m
 A ------v------- B ======================= C
 ^   4 m   D 2 m  ^        4 m (2EI)
   (EI)

Step 1: Reactions and bending moments

Moments about B: RA×6=24×2−40×2R_A\times6 = 24\times2 - 40\times2, so RA=−5.333R_A = -5.333 kN (downward); RB=24+40+5.333=69.33R_B = 24 + 40 + 5.333 = 69.33 kN.

MD=−5.333×4=−21.33 kNm,MB=−5.333×6−24×2=−80 kNm (hogging)M_D = -5.333\times4 = -21.33\ \text{kNm},\qquad M_B = -5.333\times6 - 24\times2 = -80\ \text{kNm (hogging)}

(Check from the overhang: MB=−10×42/2=−80M_B = -10\times4^2/2 = -80 kNm.)

Step 2: M/EIM/EI diagram (hogging, so conjugate loads act upward)

PortionM/EIM/EIArea (units 1/EI1/EI)Centroid
A-D triangle0 to 21.3312×4×21.33=42.67\tfrac12\times4\times21.33 = 42.672.667 m from A
D-B: rectangle21.332×21.33=42.672\times21.33 = 42.675.0 m from A
D-B: triangle0 to 58.6712×2×58.67=58.67\tfrac12\times2\times58.67 = 58.675.333 m from A
B-C (parabola, 2EI2EI)5s22EI\dfrac{5s^2}{2EI}, ss from C; 40 at B13×4×40=53.33\tfrac13\times4\times40 = 53.333 m from C

Step 3: Conjugate beam

Real hinge A stays a hinge; the interior support B becomes an internal hinge; the free end C becomes a fixed end.

Moment about the hinge B of the part AB (moment of the conjugate beam at B = 0):

RA′×6=42.67(6−2.667)+42.67(6−5)+58.67(6−5.333)=142.2+42.67+39.11=224R'_A\times6 = 42.67(6-2.667) + 42.67(6-5) + 58.67(6-5.333) = 142.2 + 42.67 + 39.11 = 224 RA′=θA=37.33EI (anticlockwise)R'_A = \theta_A = \frac{37.33}{EI}\ \text{(anticlockwise)}

Step 4: Slope at C (shear at fixed end C)

Total upward load on AB =42.67+42.67+58.67=144= 42.67 + 42.67 + 58.67 = 144; shear at B (continuous through the internal hinge):

θB=37.33−144=−106.67EI\theta_B = 37.33 - 144 = -\frac{106.67}{EI}

Shear at C: θC=−106.67−53.33=−160EI\theta_C = -106.67 - 53.33 = -\dfrac{160}{EI}

Step 5: Deflection at C (moment at fixed end C)

yC=θB×4+(−53.33)(3)=−426.67−160=−586.67EIy_C = \theta_B\times4 + (-53.33)(3) = -426.67 - 160 = -\frac{586.67}{EI}

The negative sign means downward.

Answer: slope at C =160/EI= 160/EI (clockwise); deflection at C =586.67/EI= 586.67/EI downward (kNm2^2 and kNm3^3 per EIEI respectively; with EIEI in kNm2^2 the answers are in rad and m).

✓ Answer checked by Claude Opus 5.5 (high effort)

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