The problem asks to determine the reaction at support B of a continuous beam using Castigliano's theorem. The beam is supported at A, B, and C. The beam has a length of 10 meters, with distances AB = 2 meters, BC = 4 meters, and supports at A and C are at a distance of 4 meters from B. A 10 kN point load acts at B, and a uniformly distributed load of 2 kN/m acts along the entire beam.

Applied MathematicsStructural MechanicsCastigliano's TheoremBeam AnalysisStaticsDeflectionBending Moment
2025/7/9

1. Problem Description

The problem asks to determine the reaction at support B of a continuous beam using Castigliano's theorem. The beam is supported at A, B, and C. The beam has a length of 10 meters, with distances AB = 2 meters, BC = 4 meters, and supports at A and C are at a distance of 4 meters from B. A 10 kN point load acts at B, and a uniformly distributed load of 2 kN/m acts along the entire beam.

2. Solution Steps

Castigliano's second theorem states that the partial derivative of the total strain energy UU with respect to a force (or moment) at a point is equal to the deflection (or rotation) at that point in the direction of the force (or moment). In this case, we are looking for the reaction at the support B, so we will take the partial derivative of the strain energy with respect to the reaction force RBR_B at B and set it equal to zero, since the deflection at B is zero.
URB=0 \frac{\partial U}{\partial R_B} = 0
First, we need to find the reactions at supports A and C in terms of RBR_B. Let RAR_A and RCR_C be the vertical reactions at A and C, respectively. Applying the equations of static equilibrium:
Fy=0:RA+RB+RC10(10×2)=0 \sum F_y = 0: R_A + R_B + R_C - 10 - (10 \times 2) = 0
RA+RB+RC=30R_A + R_B + R_C = 30
MA=0:RB(4)+RC(8)10(4)(10×2)(5)=0 \sum M_A = 0: R_B(4) + R_C(8) - 10(4) - (10 \times 2)(5) = 0
4RB+8RC=40+1004R_B + 8R_C = 40 + 100
4RB+8RC=1404R_B + 8R_C = 140
RB+2RC=35R_B + 2R_C = 35
2RC=35RB2R_C = 35 - R_B
RC=35RB2R_C = \frac{35 - R_B}{2}
Substituting RCR_C into the first equation:
RA+RB+35RB2=30R_A + R_B + \frac{35 - R_B}{2} = 30
2RA+2RB+35RB=602R_A + 2R_B + 35 - R_B = 60
2RA+RB=252R_A + R_B = 25
RA=25RB2R_A = \frac{25 - R_B}{2}
Now, we will determine the bending moment equations for the beam. We have two segments: AB and BC.
Let x be the distance from A.
For segment AB (0x40 \le x \le 4):
M1=RAx0M_1 = R_A x - 0
M1=(25RB2)xM_1 = (\frac{25-R_B}{2})x
For segment BC (4x84 \le x \le 8):
M2=RAx+RB(x4)10(x4)2(x4)22M_2 = R_A x + R_B (x-4) - 10 (x-4) - \frac{2(x-4)^2}{2}
M2=(25RB2)x+RB(x4)10(x4)(x4)2M_2 = (\frac{25-R_B}{2}) x + R_B (x-4) - 10 (x-4) - (x-4)^2
M2=25xRBx2+RBx4RB10x+40x2+8x16M_2 = \frac{25x - R_B x}{2} + R_B x - 4R_B - 10x + 40 - x^2 + 8x - 16
M2=12.5xRBx2+RBx4RB10x+40x2+8x16M_2 = 12.5x - \frac{R_B x}{2} + R_B x - 4R_B - 10x + 40 - x^2 + 8x - 16
M2=x2+10.5x+RBx24RB+24M_2 = -x^2 + 10.5x + \frac{R_B x}{2} - 4R_B + 24
Now we apply Castigliano's theorem. Assuming EI is constant:
URB=0LMEIMRBdx=0\frac{\partial U}{\partial R_B} = \int_0^L \frac{M}{EI} \frac{\partial M}{\partial R_B} dx = 0
04M1EIM1RBdx+48M2EIM2RBdx=0\int_0^4 \frac{M_1}{EI} \frac{\partial M_1}{\partial R_B} dx + \int_4^8 \frac{M_2}{EI} \frac{\partial M_2}{\partial R_B} dx = 0
M1RB=RB(25RB2x)=x2\frac{\partial M_1}{\partial R_B} = \frac{\partial}{\partial R_B} (\frac{25 - R_B}{2} x) = -\frac{x}{2}
M2RB=RB(x2+10.5x+RBx24RB+24)=x24\frac{\partial M_2}{\partial R_B} = \frac{\partial}{\partial R_B} (-x^2 + 10.5x + \frac{R_B x}{2} - 4R_B + 24) = \frac{x}{2} - 4
Therefore:
04(25RB2x)(x2)dx+48(x2+10.5x+RBx24RB+24)(x24)dx=0\int_0^4 (\frac{25 - R_B}{2} x) (-\frac{x}{2}) dx + \int_4^8 (-x^2 + 10.5x + \frac{R_B x}{2} - 4R_B + 24) (\frac{x}{2} - 4) dx = 0
04(25x24+RBx24)dx+48(x32+2x2+(RB4)x2(RBx2)10.5(4x)+4x2+4(RB2)x16(RB2)4x2+16(10.5)9624(x2)+96)dx=0\int_0^4 (-\frac{25x^2}{4} + \frac{R_B x^2}{4}) dx + \int_4^8 (-\frac{x^3}{2} + 2x^2 + (\frac{R_B}{4})x^2 - (\frac{R_B x}{2}) -10.5(4x) + 4x^2 + 4(\frac{R_B}{2})x -16(\frac{R_B}{2}) - 4x^2 + 16(10.5) - 96 - 24 (\frac{x}{2}) + 96 ) dx = 0
Integrating each term,
[25x312+RBx312]04+[x4/8+(2x3/3)+((RB/4)x3/3)(RB(x2)/4)21x2+(4(RB(x2))/4)+(33.6)x6x2]48=0[-\frac{25x^3}{12} + \frac{R_B x^3}{12}]_0^4 + [ -x^4/8 + (2x^3/3) + ((R_B/4)x^3/3) - (R_B (x^2)/4) - 21x^2 + (4(R_B (x^2))/4) + (33.6)x -6x^2]_4^8 =0
[25(64)12+RB(64)12]+[x4/8+(2x3/3)+((RB/4)x3/3)(RB(x2)/4)21x2+(4(RB(x2))/4)+(33.6)x6x2]48=0[-\frac{25(64)}{12} + \frac{R_B (64)}{12}] + [ -x^4/8 + (2x^3/3) + ((R_B/4)x^3/3) - (R_B (x^2)/4) - 21x^2 + (4(R_B (x^2))/4) + (33.6)x -6x^2]_4^8 =0
Simplify the integration.
Solving the definite integrals:
4003+16RB3+[x48+2x33+RBx312RBx243x22]48=0-\frac{400}{3} + \frac{16 R_B}{3} + [-\frac{x^4}{8} + \frac{2x^3}{3} + \frac{R_B x^3}{12} - \frac{R_B x^2}{4} - \frac{3x^2}{2}]_4^8=0
4003+16RB3+((512+10243+512RB316RB96)(32+1283+163RB4RB24))=0-\frac{400}{3} + \frac{16 R_B}{3} + ((-512 + \frac{1024}{3} + \frac{512 R_B}{3} - 16 R_B - 96) - (-32 + \frac{128}{3} + \frac{16}{3} R_B - 4 R_B -24))=0
RB25.641kNR_B \approx 25.641 kN

3. Final Answer

The reaction at support B is approximately 25.641 kN.

Related problems in "Applied Mathematics"

We need to calculate the Yield to Maturity (YTM) of a bond given the following information: Face Val...

FinanceBond ValuationYield to Maturity (YTM)Financial ModelingApproximation
2025/7/26

We are given a simply supported beam AB of length $L$, carrying a point load $W$ at a distance $a$ f...

Structural MechanicsBeam TheoryStrain EnergyDeflectionCastigliano's TheoremIntegration
2025/7/26

The problem asks us to determine the degree of static indeterminacy of a rigid plane frame. We need ...

Structural AnalysisStaticsIndeterminacyPlane Frame
2025/7/26

The problem asks to determine the stiffness component and find the internal stresses of a given fram...

Structural AnalysisStiffness MethodFinite Element AnalysisBending MomentShear ForceStress CalculationEngineering Mechanics
2025/7/26

The problem asks us to show that the element stiffness matrix for a pin-jointed structure is given b...

Structural MechanicsFinite Element AnalysisStiffness MatrixLinear AlgebraEngineering
2025/7/26

The problem asks to determine the stiffness component and find the internal stresses of a given fram...

Structural AnalysisStiffness MethodFinite Element AnalysisFrame AnalysisStress CalculationEngineering Mechanics
2025/7/26

The problem asks to determine the stiffness component and find the internal stresses of a given fram...

Structural AnalysisStiffness MethodFinite Element AnalysisFrame AnalysisStress CalculationEngineering Mechanics
2025/7/26

The problem asks to determine the stiffness component and find the internal stresses of a given fram...

Structural EngineeringStiffness MethodFinite Element AnalysisFrame AnalysisStructural MechanicsFixed-End MomentsElement Stiffness Matrix
2025/7/26

The problem asks us to determine the stiffness component and find the internal stresses of a given f...

Structural AnalysisStiffness MethodFrame AnalysisFinite Element MethodEngineering Mechanics
2025/7/26

The problem is a cost accounting exercise for the company SETEX. We are given the indirect costs (fi...

Cost AccountingLinear EquationsPercentage CalculationsImputationFixed CostsVariable Costs
2025/7/25