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 three supports (A, B, and C). There is a point load of 10 kN acting between support A and B and a uniformly distributed load of 2 kN/m acting between support B and C. The distances between the supports and loads are specified: 4 m between A and the point load, 2 m between the point load and B, and 4 m between B and C.

Applied MathematicsStructural MechanicsCastigliano's TheoremBeam AnalysisStaticsStrain EnergyMacaulay's Method
2025/7/9

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 three supports (A, B, and C). There is a point load of 10 kN acting between support A and B and a uniformly distributed load of 2 kN/m acting between support B and C. The distances between the supports and loads are specified: 4 m between A and the point load, 2 m between the point load and B, and 4 m between B and C.

2. Solution Steps

To determine the support reactions using Castigliano's theorem, we need to find the strain energy of the beam and then differentiate it with respect to the reactions. Because the beam has multiple supports, it's statically indeterminate. We can assume that the reactions at A and C are the redundants.
Let RAR_A, RBR_B, and RCR_C be the reactions at supports A, B, and C, respectively.
Let's consider the beam as two sections AB and BC.
Section AB:
The length of the section is 4+2=64 + 2 = 6 m. The point load is at 4 m from A.
Let's express the bending moment M1(x)M_1(x) at any point xx from A in section AB (where 0x60 \le x \le 6):
M1(x)=RAx10<x4>M_1(x) = R_A x - 10 <x-4>
where <xa><x-a> is the Macaulay bracket, which is zero if x<ax < a and equals (xa)(x-a) if x>ax > a.
Section BC:
The length of the section is 4 m.
Let's express the bending moment M2(x)M_2(x) at any point xx from C in section BC (where 0x40 \le x \le 4):
M2(x)=RCx2x22=RCxx2M_2(x) = R_C x - \frac{2x^2}{2} = R_C x - x^2
The reaction at B can be determined using the equilibrium equation for the entire beam:
RA+RB+RC=10+24=18R_A + R_B + R_C = 10 + 2*4 = 18
RB=18RARCR_B = 18 - R_A - R_C
Using Castigliano's theorem:
The deflection at the supports A and C is zero.
URA=0\frac{\partial U}{\partial R_A} = 0 and URC=0\frac{\partial U}{\partial R_C} = 0
The strain energy UU in the beam due to bending is given by:
U=0LM22EIdxU = \int_0^L \frac{M^2}{2EI} dx
where M is the bending moment, E is Young's modulus, and I is the moment of inertia.
Since URA=0\frac{\partial U}{\partial R_A} = 0, we have:
06M1EIM1RAdx+04M2EIM2RAdx=0\int_0^6 \frac{M_1}{EI} \frac{\partial M_1}{\partial R_A} dx + \int_0^4 \frac{M_2}{EI} \frac{\partial M_2}{\partial R_A} dx = 0
M1RA=x\frac{\partial M_1}{\partial R_A} = x
M2RA=0\frac{\partial M_2}{\partial R_A} = 0
So, we have:
06M1xdx=0\int_0^6 M_1 x dx = 0
06(RAx10<x4>)xdx=0\int_0^6 (R_A x - 10 <x-4>) x dx = 0
06(RAx210x<x4>)dx=0\int_0^6 (R_A x^2 - 10x <x-4>) dx = 0
RA06x2dx1046x(x4)dx=0R_A \int_0^6 x^2 dx - 10 \int_4^6 x(x-4) dx = 0
RA[x33]061046(x24x)dx=0R_A [\frac{x^3}{3}]_0^6 - 10 \int_4^6 (x^2 - 4x) dx = 0
RA(633)10[x332x2]46=0R_A (\frac{6^3}{3}) - 10 [\frac{x^3}{3} - 2x^2]_4^6 = 0
72RA10[(2163236)(643216)]=072 R_A - 10 [(\frac{216}{3} - 2*36) - (\frac{64}{3} - 2*16)] = 0
72RA10[(7272)(64332)]=072 R_A - 10 [(72-72) - (\frac{64}{3} - 32)] = 0
72RA10[0(64963)]=072 R_A - 10 [0 - (\frac{64-96}{3})] = 0
72RA10(323)=072 R_A - 10 (\frac{32}{3}) = 0
72RA=320372 R_A = \frac{320}{3}
RA=320372=320216=4027R_A = \frac{320}{3*72} = \frac{320}{216} = \frac{40}{27} kN
Similarly, since URC=0\frac{\partial U}{\partial R_C} = 0, we have:
06M1EIM1RCdx+04M2EIM2RCdx=0\int_0^6 \frac{M_1}{EI} \frac{\partial M_1}{\partial R_C} dx + \int_0^4 \frac{M_2}{EI} \frac{\partial M_2}{\partial R_C} dx = 0
M1RC=0\frac{\partial M_1}{\partial R_C} = 0
M2RC=x\frac{\partial M_2}{\partial R_C} = x
So, we have:
04M2xdx=0\int_0^4 M_2 x dx = 0
04(RCxx2)xdx=0\int_0^4 (R_C x - x^2) x dx = 0
04(RCx2x3)dx=0\int_0^4 (R_C x^2 - x^3) dx = 0
RC04x2dx04x3dx=0R_C \int_0^4 x^2 dx - \int_0^4 x^3 dx = 0
RC[x33]04[x44]04=0R_C [\frac{x^3}{3}]_0^4 - [\frac{x^4}{4}]_0^4 = 0
RC(433)444=0R_C (\frac{4^3}{3}) - \frac{4^4}{4} = 0
RC643=2564=64R_C \frac{64}{3} = \frac{256}{4} = 64
RC=64364=3R_C = \frac{64 * 3}{64} = 3 kN
RB=18RARC=1840273=154027=4054027=36527R_B = 18 - R_A - R_C = 18 - \frac{40}{27} - 3 = 15 - \frac{40}{27} = \frac{405 - 40}{27} = \frac{365}{27} kN

3. Final Answer

RA=4027R_A = \frac{40}{27} kN
RB=36527R_B = \frac{365}{27} kN
RC=3R_C = 3 kN

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