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Castigliano: beam, redundant moment at A

Short answer

Release rotation at fixed end A, take clockwise MA as redundant. RA = –(MA+13)/4, ∂M/∂MA = 1 – x/4. Set∫₀⁴ M(1–x/4)dx=0 yields 4MA/3–26/3+5=0, so MA=2.75 kNm. Then RA=–3.94 kN downward, RC=9.94 kN upward.

Analyze the given loaded beam using Castigliano's theorem. The redundant should be considered as the support moment at A. EI constant. [Figure: beam ABCD, A fixed; 10 kNm moment applied at B (2 m from A); support at C, 2 m from B; 6 kN/m UDL on overhang CD of 1 m.]

Reading of the figure: A fixed; B is 2 m from A where a couple of 10 kNm (taken clockwise) is applied; C is a roller 2 m from B; CD is a 1 m overhang with 6 kN/m. EI is constant.

The fixity at A gives one redundant. Release the rotation at A and take the fixed-end moment MAM_A (clockwise on the beam) as the redundant, so the beam becomes simply supported at A and C with an overhang. The condition is that the slope at A is zero:

∂U∂MA=θA=0\frac{\partial U}{\partial M_A} = \theta_A = 0
            10 kNm (cw)        6 kN/m
 A ||--------B--------C vvvvvvvv D
 (fixed)              ^ (roller)
 |<-- 2 -->|<-- 2 -->|<-- 1 -->|

Reaction at A in terms of MAM_A

Moments about C (the overhang load is 6 kN at 0.5 m from C):

4RA+MA+10+6(0.5)=0 ⇒ RA=−MA+1344R_A + M_A + 10 + 6(0.5) = 0 \ \Rightarrow\ R_A = -\frac{M_A + 13}{4}

∂RA∂MA=−14\dfrac{\partial R_A}{\partial M_A} = -\dfrac{1}{4} (RAR_A is positive upward).

Bending moments (x from A, sagging positive)

0≤x≤2:M=MA+RAx,∂M∂MA=1−x42≤x≤4:M=MA+RAx+10,∂M∂MA=1−x4\begin{aligned} 0 \le x \le 2:\quad M &= M_A + R_A x, & \frac{\partial M}{\partial M_A} &= 1 - \frac{x}{4} \\ 2 \le x \le 4:\quad M &= M_A + R_A x + 10, & \frac{\partial M}{\partial M_A} &= 1 - \frac{x}{4} \end{aligned}

The overhang CD does not depend on MAM_A (its moment comes from the UDL alone), so it adds nothing to the integral.

Castigliano's theorem

∫04M(1−x4)dx=0\int_0^4 M\left(1-\frac{x}{4}\right)dx = 0

Evaluating each term with M=MA−(MA+13)x4+10 [x>2]M = M_A - \dfrac{(M_A+13)x}{4} + 10\,[x>2]:

MA∫04(1−x4)2dx=43MA−134∫04x(1−x4)dx=−134⋅83=−26310∫24(1−x4)dx=10(0.5)=5\begin{aligned} M_A\int_0^4\left(1-\tfrac{x}{4}\right)^2dx &= \tfrac{4}{3}M_A \\ -\tfrac{13}{4}\int_0^4 x\left(1-\tfrac{x}{4}\right)dx &= -\tfrac{13}{4}\cdot\tfrac{8}{3} = -\tfrac{26}{3} \\ 10\int_2^4 \left(1-\tfrac{x}{4}\right)dx &= 10(0.5) = 5 \end{aligned} 43MA−263+5=0 ⇒ MA=114=2.75 kNm\tfrac{4}{3}M_A - \tfrac{26}{3} + 5 = 0 \ \Rightarrow\ M_A = \tfrac{11}{4} = 2.75\ \text{kNm}

Other reactions

RA=−2.75+134=−3.9375 kN (downward),RC=6−(−3.9375)=9.9375 kN (↑)R_A = -\frac{2.75+13}{4} = -3.9375\ \text{kN}\ (\text{downward}), \qquad R_C = 6 - (-3.9375) = 9.9375\ \text{kN}\ (\uparrow)

Bending moments (kNm)

PointBM
A+2.75 (sagging)
B (left of couple)-5.125
B (right of couple)+4.875
C-3.000
D0

Answer: MA=2.75M_A = 2.75 kNm (clockwise on the beam, provided by the wall), RA=3.938R_A = 3.938 kN downward, RC=9.938R_C = 9.938 kN upward.

✓ Answer checked by Claude Opus 5.5 (high effort)

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