The problem asks us to determine the reaction at support B of a continuous beam using Castigliano's theorem. The beam is supported at A, B, and C. It is subjected to a 10 kN load located 4m from support A, and a 2 kN load located 6m from support A (or 4m from support B, 1m from support C). The distances between supports are: AB = 6m (4+2) and BC = 5m (4+1).

Applied MathematicsStructural EngineeringCastigliano's TheoremBeam DeflectionBending MomentIntegration
2025/7/9

1. Problem Description

The problem asks us to determine the reaction at support B of a continuous beam using Castigliano's theorem. The beam is supported at A, B, and C. It is subjected to a 10 kN load located 4m from support A, and a 2 kN load located 6m from support A (or 4m from support B, 1m from support C). The distances between supports are: AB = 6m (4+2) and BC = 5m (4+1).

2. Solution Steps

Castigliano's second theorem states that the partial derivative of the total strain energy UU with respect to a force PP is equal to the displacement at the point of application of the force in the direction of the force. Mathematically, UP=Δ\frac{\partial U}{\partial P} = \Delta. For supports, we seek the reaction force, and the displacement is zero. Thus URB=0\frac{\partial U}{\partial R_B} = 0. We'll assume constant EI. The strain energy UU is given by:
U=M22EIdxU = \int \frac{M^2}{2EI} dx
Therefore, URB=2M2EIMRBdx=1EIMMRBdx=0\frac{\partial U}{\partial R_B} = \int \frac{2M}{2EI} \frac{\partial M}{\partial R_B} dx = \frac{1}{EI} \int M \frac{\partial M}{\partial R_B} dx = 0
Since EI is constant and not zero, we need to find the bending moment M as a function of x, then take its partial derivative with respect to RBR_B, and finally integrate MMRBM \frac{\partial M}{\partial R_B} over the length of the beam. We will consider two sections: Section 1: AB and Section 2: BC.
First, we need to determine the support reactions. Let's denote the vertical reactions at A, B, and C as RAR_A, RBR_B, and RCR_C, respectively. Taking the sum of vertical forces to be zero gives:
RA+RB+RC=10+2=12R_A + R_B + R_C = 10 + 2 = 12
Taking moments about point A:
6RB+11RC=104+26=40+12=526R_B + 11R_C = 10*4 + 2*6 = 40 + 12 = 52
Now, we introduce a dummy variable RBR_B at support B.
For section AB (0 <= x <= 6), taking moments about the cut at a distance x from A:
M1(x)=RAx10x41M_1(x) = R_A x - 10 \langle x - 4 \rangle^1, where xan\langle x - a \rangle^n is the Macaulay bracket, equal to (xa)n(x-a)^n when x>ax > a and 0 when x<ax < a.
For section BC (0 <= x' <= 5), taking moments about the cut at a distance x' from C:
M2(x)=RCx2xM_2(x') = R_C x' - 2x', where x' is the distance from C. Note that x=11xx' = 11 - x.
RA+RB+RC=12R_A + R_B + R_C = 12
6RB+11RC=526R_B + 11R_C = 52
RA=12RBRCR_A = 12 - R_B - R_C
RC=(526RB)/11R_C = (52 - 6R_B) / 11
RA=12RB(526RB)/11=(13211RB52+6RB)/11=(805RB)/11R_A = 12 - R_B - (52 - 6R_B) / 11 = (132 - 11R_B - 52 + 6R_B) / 11 = (80 - 5R_B) / 11
M1(x)=(805RB)11x10x41M_1(x) = \frac{(80 - 5R_B)}{11}x - 10 \langle x - 4 \rangle^1
M2(x)=(526RB)11x2xM_2(x') = \frac{(52 - 6R_B)}{11}x' - 2x'
M1RB=5x11\frac{\partial M_1}{\partial R_B} = \frac{-5x}{11}
M2RB=6x11\frac{\partial M_2}{\partial R_B} = \frac{-6x'}{11}
06((805RB)11x10x41)(5x11)dx+05((526RB)11x2x)(6x11)dx=0\int_0^6 (\frac{(80 - 5R_B)}{11}x - 10 \langle x - 4 \rangle^1) (\frac{-5x}{11}) dx + \int_0^5 (\frac{(52 - 6R_B)}{11}x' - 2x') (\frac{-6x'}{11}) dx' = 0
06(400x2+25RBx2121+50x11x41)dx+05(312x2+36RBx2+132x2121)dx=0\int_0^6 (\frac{-400x^2 + 25R_B x^2}{121} + \frac{50x}{11}\langle x - 4 \rangle^1) dx + \int_0^5 (\frac{-312x'^2 + 36R_B x'^2 + 132x'^2}{121}) dx' = 0
06(400x2+25RBx2121+50x11(x4))dx\int_0^6 (\frac{-400x^2 + 25R_B x^2}{121} + \frac{50x}{11}(x - 4)) dx from 4 to 6 +05(180x2+36RBx2121)dx=0+ \int_0^5 (\frac{-180x'^2 + 36R_B x'^2}{121}) dx' = 0
(400x3/3+25RBx3/3121)06+(50(x3/32x2)11)46+(180x3/3+36RBx3/3121)05=0(\frac{-400x^3/3 + 25R_B x^3/3}{121})|_0^6 + (\frac{50(x^3/3 - 2x^2)}{11})|_4^6 + (\frac{-180x'^3/3 + 36R_B x'^3/3}{121})|_0^5 = 0
(400216/3+25RB216/3121)+(50(216/3236)50(64/3216)11)+(180125/3+36RB125/3121)=0(\frac{-400*216/3 + 25R_B *216/3}{121}) + (\frac{50(216/3 - 2*36) - 50(64/3 - 2*16)}{11}) + (\frac{-180*125/3 + 36R_B *125/3}{121}) = 0
(28800+1800RB121)+(50(7272)50(64/332)11)+(7500+1500RB121)=0(\frac{-28800 + 1800R_B}{121}) + (\frac{50(72 - 72) - 50(64/3 - 32)}{11}) + (\frac{-7500 + 1500R_B}{121}) = 0
(28800+1800RB121)+(050(64/396/3)11)+(7500+1500RB121)=0(\frac{-28800 + 1800R_B}{121}) + (\frac{0 - 50(64/3 - 96/3)}{11}) + (\frac{-7500 + 1500R_B}{121}) = 0
(28800+1800RB121)+(50(32/3)11)+(7500+1500RB121)=0(\frac{-28800 + 1800R_B}{121}) + (\frac{-50(-32/3)}{11}) + (\frac{-7500 + 1500R_B}{121}) = 0
(28800+1800RB121)+(1600/311)+(7500+1500RB121)=0(\frac{-28800 + 1800R_B}{121}) + (\frac{1600/3}{11}) + (\frac{-7500 + 1500R_B}{121}) = 0
(28800+1800RB121)+(160033)+(7500+1500RB121)=0(\frac{-28800 + 1800R_B}{121}) + (\frac{1600}{33}) + (\frac{-7500 + 1500R_B}{121}) = 0
Multiplying by 121:
28800+1800RB+1600121/337500+1500RB=0-28800 + 1800R_B + 1600*121/33 - 7500 + 1500R_B = 0
36300+3300RB+160011/3=0-36300 + 3300R_B + 1600 * 11 / 3 = 0
3300RB=3630017600/33/3=(10890017600)/3=91300/33300R_B = 36300 - 17600/3 * 3/3 = (108900-17600)/3 = 91300/3
RB=(91300/3)/3300=91300/(33300)=91300/9900=913/999.22R_B = (91300/3) / 3300 = 91300/(3*3300) = 91300 / 9900 = 913 / 99 \approx 9.22

3. Final Answer

RB9.22kNR_B \approx 9.22 kN

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