The problem asks to determine the reactions at the supports of a given structure using Castigliano's theorem. The structure is a continuous beam with supports at A, B, and C. There is a 10 kN point load and a 2 kN/m uniformly distributed load. The lengths of the segments are 4m, 2m, and 4m, respectively.

Applied MathematicsStructural AnalysisCastigliano's TheoremStrain EnergyIndeterminate StructuresBeam Deflection
2025/7/10

1. Problem Description

The problem asks to determine the reactions at the supports of a given structure using Castigliano's theorem. The structure is a continuous beam with supports at A, B, and C. There is a 10 kN point load and a 2 kN/m uniformly distributed load. The lengths of the segments are 4m, 2m, and 4m, respectively.

2. Solution Steps

Castigliano's second theorem states that the partial derivative of the total strain energy UU with respect to a force PiP_i applied at a point is equal to the displacement δi\delta_i at that point in the direction of the force:
δi=UPi\delta_i = \frac{\partial U}{\partial P_i}
For finding reactions at supports, the displacement is zero. Thus,
Ri=UΔi=0R_i = \frac{\partial U}{\partial \Delta_i} = 0
where RiR_i is the reaction force at support ii and Δi\Delta_i is the displacement at support ii (which is zero). This means that the derivative of the strain energy with respect to the redundant reaction is zero.
The total strain energy UU for a beam is given by:
U=M22EIdxU = \int \frac{M^2}{2EI} dx
Where MM is the bending moment as a function of xx, EE is the modulus of elasticity, and II is the moment of inertia.
To solve this indeterminate problem, we can consider RBR_B as the redundant reaction at support B. We can express the bending moment MM as a function of xx and RBR_B. Then, we can apply Castigliano's theorem:
URB=2M2EIMRBdx=MEIMRBdx=0\frac{\partial U}{\partial R_B} = \int \frac{2M}{2EI} \frac{\partial M}{\partial R_B} dx = \int \frac{M}{EI} \frac{\partial M}{\partial R_B} dx = 0
Since EIEI is constant, it can be taken out of the integral:
MMRBdx=0\int M \frac{\partial M}{\partial R_B} dx = 0
Let's define the sections of the beam:
Section 1: A to point load (0 <= x <= 4)
Section 2: Point load to B (0 <= x <= 2)
Section 3: B to C (0 <= x <= 4)
RA+RB+RC=10+2(10)=30R_A + R_B + R_C = 10 + 2(10) = 30
RA(10)+RB(6)=10(2)+2(10)(5)=20+100=120R_A(10) + R_B(6) = 10(2) + 2(10)(5) = 20 + 100 = 120
Solving for RAR_A:
RA=1206RB10=120.6RBR_A = \frac{120 - 6 R_B}{10} = 12 - 0.6 R_B
Solving for RCR_C:
RC=30RARB=30(120.6RB)RB=180.4RBR_C = 30 - R_A - R_B = 30 - (12 - 0.6 R_B) - R_B = 18 - 0.4 R_B
Section 1 (0 <= x <= 4):
M1=RAx=(120.6RB)xM_1 = R_A x = (12 - 0.6 R_B) x
M1RB=0.6x\frac{\partial M_1}{\partial R_B} = -0.6x
Section 2 (0 <= x <= 2): x is measured from the 10kN point load
M2=RA(4+x)10x=(120.6RB)(4+x)10x=48+12x2.4RB0.6RBx10x=48+2x2.4RB0.6RBxM_2 = R_A(4+x) - 10x = (12 - 0.6R_B)(4+x) - 10x = 48 + 12x - 2.4R_B - 0.6R_Bx - 10x = 48 + 2x - 2.4 R_B - 0.6 R_B x
M2RB=2.40.6x\frac{\partial M_2}{\partial R_B} = -2.4 - 0.6x
Section 3 (0 <= x <= 4):
M3=RCx+2x2/2=(180.4RB)x+x2=18x0.4RBx+x2M_3 = R_C x + 2*x^2 /2 = (18-0.4R_B)x + x^2= 18x - 0.4 R_B x + x^2
M3RB=0.4x\frac{\partial M_3}{\partial R_B} = -0.4x
Now, we can set up the integral:
04(120.6RB)x(0.6x)dx+02(48+2x2.4RB0.6RBx)(2.40.6x)dx+04(18x0.4RBx+x2)(0.4x)dx=0\int_0^4 (12-0.6R_B)x(-0.6x) dx + \int_0^2 (48 + 2x - 2.4R_B - 0.6 R_B x)(-2.4 - 0.6x) dx + \int_0^4 (18x - 0.4R_Bx + x^2)(-0.4x) dx = 0
Integrating each part:
(0.6)04(12x20.6RBx2)dx+02[(48+2x)(2.40.6x)+(2.4RB0.6RBx)(2.40.6x)]dx+(0.4)04(18x20.4RBx2+x3)dx=0(-0.6) \int_0^4 (12x^2 - 0.6 R_B x^2) dx + \int_0^2 [(48+2x)(-2.4-0.6x)+(-2.4R_B - 0.6 R_B x)(-2.4 - 0.6x)] dx + (-0.4) \int_0^4 (18x^2 - 0.4 R_B x^2 + x^3) dx = 0
(0.6)[12x330.6RBx33]04+02[115.228.8x4.8x1.2x2+5.76RB+1.44RBx+1.44RBx+0.36RBx2]dx+(0.4)[18x330.4RBx33+x44]04=0(-0.6) [\frac{12x^3}{3} - \frac{0.6R_B x^3}{3}]_0^4 + \int_0^2 [-115.2 - 28.8x - 4.8x - 1.2x^2 + 5.76R_B + 1.44 R_B x + 1.44 R_B x + 0.36 R_B x^2] dx + (-0.4)[\frac{18x^3}{3} - \frac{0.4 R_B x^3}{3} + \frac{x^4}{4}]_0^4 = 0
(0.6)[4(4)30.2RB(4)3]+02[115.233.6x1.2x2+5.76RB+2.88RBx+0.36RBx2]dx+(0.4)[6(4)30.4RB(4)33+(4)44]=0(-0.6) [4(4)^3 - 0.2 R_B (4)^3] + \int_0^2 [-115.2 - 33.6x - 1.2x^2 + 5.76 R_B + 2.88 R_B x + 0.36 R_B x^2] dx + (-0.4)[6(4)^3 - \frac{0.4 R_B (4)^3}{3} + \frac{(4)^4}{4}] = 0
(0.6)[25612.8RB]+[115.2x33.6x221.2x33+5.76RBx+2.88RBx22+0.36RBx33]02+(0.4)[3848.533RB+64]=0(-0.6) [256 - 12.8 R_B] + [-115.2x - \frac{33.6x^2}{2} - \frac{1.2x^3}{3} + 5.76 R_B x + \frac{2.88 R_B x^2}{2} + \frac{0.36 R_B x^3}{3}]_0^2 + (-0.4) [384 - 8.533 R_B + 64] = 0
153.6+7.68RB+[115.2(2)16.8(22)0.4(23)+5.76RB(2)+1.44RB(22)+0.12RB(23)]0.4[4488.533RB]=0-153.6 + 7.68 R_B + [-115.2(2) - 16.8(2^2) - 0.4(2^3) + 5.76 R_B (2) + 1.44 R_B (2^2) + 0.12 R_B (2^3)] - 0.4[448 - 8.533 R_B] = 0
153.6+7.68RB+[230.467.23.2+11.52RB+5.76RB+0.96RB]179.2+3.413RB=0-153.6 + 7.68 R_B + [-230.4 - 67.2 - 3.2 + 11.52 R_B + 5.76 R_B + 0.96 R_B] - 179.2 + 3.413 R_B = 0
153.6+7.68RB300.8+18.24RB179.2+3.413RB=0-153.6 + 7.68 R_B -300.8 + 18.24 R_B - 179.2 + 3.413 R_B = 0
633.6+29.333RB=0-633.6 + 29.333 R_B = 0
RB=633.629.333=21.60 kNR_B = \frac{633.6}{29.333} = 21.60 \text{ kN}
RA=120.6(21.60)=1212.96=0.96 kNR_A = 12 - 0.6(21.60) = 12 - 12.96 = -0.96 \text{ kN}
RC=180.4(21.60)=188.64=9.36 kNR_C = 18 - 0.4(21.60) = 18 - 8.64 = 9.36 \text{ kN}

3. Final Answer

RA=0.96 kNR_A = -0.96 \text{ kN}
RB=21.60 kNR_B = 21.60 \text{ kN}
RC=9.36 kNR_C = 9.36 \text{ kN}

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