---
title: "Castigliano: propped cantilever, moment and rotation"
subject: "Theory of Structures II"
chapter: 2
key: "semester_5/theory_of_structures_ii:castigliano-propped-30knm-50kn-moment-rotation"
source: https://www.bctengineer.com/q/semester_5/theory_of_structures_ii/castigliano-propped-30knm-50kn-moment-rotation
site: BCT Engineering
---

# Castigliano: propped cantilever, moment and rotation

Theory of Structures II · Chapter 2: Force method

- Asked in: 2076 Asoj, 10 marks
- Video: [Castigliano's theorem numerical | Find rotation at B | PU 2021, TU 2075,2076,2071 | most important](https://www.youtube.com/watch?v=uRARqSlQ-gQ) — Sudip Dhakal
- Answer checked by Claude Opus 5.5 (high effort) on 2026-10-14
- Page: https://www.bctengineer.com/q/semester_5/theory_of_structures_ii/castigliano-propped-30knm-50kn-moment-rotation
- Whole chapter: https://www.bctengineer.com/md/semester_5/theory_of_structures_ii/chapter-2

## Question

Determine the moment at the fixed support and the rotation at the roller support of a propped cantilever beam of span 10 m loaded with a uniformly distributed load of 30 kN/m on its whole span and a point load of 50 kN at the centre using Castigliano's theorem.

## Short answer

Taking the roller reaction as redundant and applying Castigliano’s theorem, the fixed-end moment is 468.75 kNm (hogging) and the roller rotation is 781.25/EI rad (anticlockwise).

## Answer

The beam AB (span 10 m) is fixed at A and has a roller at B. Loads: 30 kN/m over the whole span and 50 kN at the centre. EI is constant. Take the roller reaction $R_B$ as the redundant.

```text
        50 kN
          v      30 kN/m
 vvvvvvvvvvvvvvvvvvvvvvvvvv
 ||==========+===========o
 A (fixed)  5 m          B (roller, R_B)
 |<------------ 10 m ---->|
```

#### Bending moment (x measured from B)
$$
M = R_B\,x - 15x^2 - 50\langle x-5\rangle, \qquad \frac{\partial M}{\partial R_B} = x
$$

#### Redundant from Castigliano
The deflection at B is zero:

$$
\frac{\partial U}{\partial R_B} = \frac{1}{EI}\int_0^{10} M\,x\,dx = 0
$$

$$
\int_0^{10}\left(R_B x^2 - 15x^3\right)dx - 50\int_5^{10}(x-5)x\,dx = 0
$$

$$
\frac{1000}{3}R_B - 37500 - 5208.33 = 0 \ \Rightarrow\ R_B = 128.125\ \text{kN}
$$

(Check: UDL alone gives $3wL/8 = 112.5$ kN and the central load gives $5P/16 = 15.625$ kN; their sum is 128.125 kN.)

#### Moment at the fixed support
$$
V_A = 350 - 128.125 = 221.875\ \text{kN}
$$

$$
M_A = R_B(10) - 30\cdot\frac{10^2}{2} - 50(5) = 128.125(10) - 1500 - 250 = -468.75\ \text{kNm}
$$

The fixed-end moment is **468.75 kNm (hogging)**.

#### Rotation at the roller B
Apply a dummy couple $M'$ at B. Then $\partial M/\partial M' = 1$ at the sections (the extra term caused by the change of $R_B$ integrates to zero because $\int M\,x\,dx = 0$), so

$$
\theta_B = \frac{\partial U}{\partial M'}\bigg|_{M'=0} = \frac{1}{EI}\int_0^{10} M\,dx
$$

$$
\int_0^{10} M\,dx = R_B\frac{10^2}{2} - 15\frac{10^3}{3} - 50\frac{5^2}{2} = 128.125(50) - 5000 - 625 = 781.25
$$

$$
\theta_B = \frac{781.25}{EI}\ \text{rad (anticlockwise)}
$$

**Answer: fixed-end moment $M_A = 468.75$ kNm (hogging); rotation at the roller $\theta_B = \dfrac{781.25}{EI}$ rad.**

## Check yourself

The answer's key points as multiple-choice questions, with the correct option and why.

1. What is the redundant and the condition that gives it?
   A. R_B at the roller; the deflection at B is zero, so dU/dR_B = 0
   B. M_A at the fixed end; slope at A equals zero
   C. R_B; the moment at B is zero
   D. V_A; the shear at A is zero
   Answer: A. Removing the roller leaves a cantilever; the roller prevents deflection at B. (Key point: Redundant and condition)

2. What is R_B and how can it be checked?
   A. 112.5 kN; the point load adds nothing
   B. 128.125 kN; UDL alone gives 3wL/8 = 112.5 kN and the point load gives 5P/16 = 15.625 kN
   C. 350 kN, the total load
   D. 75 kN, half of the UDL
   Answer: B. By superposition the propped-cantilever reactions add up to 128.125 kN. (Key point: Value of R_B)

3. What is the moment at the fixed support?
   A. 375 kNm hogging
   B. 1750 kNm hogging
   C. 468.75 kNm hogging
   D. 250 kNm hogging
   Answer: C. M_A = 128.125 x 10 - 30 x 10^2/2 - 50 x 5 = -468.75 kNm. The value 375 would be for the UDL alone. (Key point: Fixed-end moment)

4. Why is a dummy couple M' applied at B, and what is theta_B?
   A. To make the beam determinate; theta_B = 0
   B. To replace the roller; theta_B = 468.75/EI
   C. To measure the deflection at B; theta_B = 128.125/EI
   D. There is no real couple at B, so M' is added to differentiate and then set to zero; theta_B = 781.25/EI
   Answer: D. dU/dM' at M' = 0 gives the rotation: (1/EI) times the integral of M dx = 781.25/EI. (Key point: Rotation at roller)

## Related in Theory of Structures II

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