---
title: "ILD: bending moment at fixed support, 10 m beam"
subject: "Theory of Structures II"
chapter: 4
key: "semester_5/theory_of_structures_ii:ild-bm-fixed-support-10m-1"
source: https://www.bctengineer.com/q/semester_5/theory_of_structures_ii/ild-bm-fixed-support-10m-1
site: BCT Engineering
---

# ILD: bending moment at fixed support, 10 m beam

Theory of Structures II · Chapter 4: Influence line (IL) for continuous beams

- Asked in: 2068 Baishakh, 10 marks
- 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/ild-bm-fixed-support-10m-1
- Whole chapter: https://www.bctengineer.com/md/semester_5/theory_of_structures_ii/chapter-4

## Question

Draw influence line diagram for bending moment at the fixed support of the beam and obtain ordinates at each 1.25 m interval. [Figure: propped cantilever, fixed at the left, roller at the right, span 10 m, EI constant.]

## Short answer

For a 10 m propped cantilever, MA = x(L-x)(2L-x)/(2L^2), hogging negative. Ordinates per unit load at 1.25 m intervals are 0, -1.0254, -1.6406, -1.9043, -1.875, -1.6113, -1.1719, -0.6152, 0; maximum about -1.925 at x = 4.22 m.

## Answer

Sign convention: sagging moment (+), hogging moment (-); shear positive when the left part tends to go up; reaction positive upward. Ordinates are for a unit load moving along the beam.

#### Method
Propped cantilever AB, span $L = 10$ m, A fixed, B roller, constant $EI$. The bending moment at the fixed support A is the reaction moment (hogging). Muller-Breslau: replace the fixed support by a hinge and apply a unit rotation at A; the deflected shape of the beam is the ILD of $M_A$.

#### Derivation of the ordinates
Take the roller reaction $R_B$ as the redundant. For a unit load at $x$ from A:
1. Deflection at B of the released cantilever (fixed at A) under the unit load: $\delta_{Bx} = \dfrac{x^2(3L-x)}{6EI}$.
2. Deflection at B under a unit upward force at B: $f_{BB} = \dfrac{L^3}{3EI}$.
3. Compatibility $\delta_{Bx} = R_Bf_{BB}$ gives $R_B = \dfrac{x^2(3L-x)}{2L^3}$.
4. Moment at A (hogging): $M_A = x\cdot 1 - R_BL = x - \dfrac{x^2(3L-x)}{2L^2} = \dfrac{x(L-x)(2L-x)}{2L^2}$.

Sample: $x = 5$: $R_B = \dfrac{25\times25}{2000} = 0.3125$, $M_A = 5 - 0.3125\times10 = 1.875$ (hogging). $x = 3.75$: $R_B = \dfrac{14.0625\times26.25}{2000} = 0.1846$, $M_A = 3.75 - 1.846 = 1.904$.

#### Ordinates (1.25 m interval, hogging = negative)
| x from A (m) | 0 | 1.25 | 2.5 | 3.75 | 5 | 6.25 | 7.5 | 8.75 | 10 |
|---|---|---|---|---|---|---|---|---|---|
| $M_A$ | 0 | -1.0254 | -1.6406 | -1.9043 | -1.875 | -1.6113 | -1.1719 | -0.6152 | 0 |

#### ILD shape
```text




**--------------------------------------------***
  **                                     *****
    ****                            *****
        *****                *******
             ****************
^                                               ^
```
The maximum ordinate is about $-1.925$ at $x = 4.22$ m ($0.42L$). A concentrated load $P$ at $x = 5$ m gives $M_A = 1.875P$ hogging; a UDL $w$ over the full span gives $M_A = w\times$ area $= wL^2/8 = 12.5w$.

## Check yourself

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

1. By the Muller-Breslau principle, how is the ILD of the moment at the fixed support A obtained?
   A. Replace the fixed support by a hinge and give a unit rotation at A; the deflected shape is the ILD.
   B. Remove the roller and apply a unit upward displacement at B.
   C. Cut the beam at A and give a unit vertical shift between the faces.
   D. Replace the fixed support by a roller and apply a unit load at A.
   Answer: A. Releasing the moment restraint (hinge) and imposing a unit rotation gives the deflected shape that is the ILD of M_A. (Key point: Muller-Breslau)

2. In the derivation, which condition gives the roller reaction R_B?
   A. Sum of vertical forces equals zero.
   B. Deflection at B of the released cantilever under the unit load equals R_B times the flexibility f_BB.
   C. Moment at B equals zero.
   D. Slope at A equals the slope at B.
   Answer: B. R_B is the redundant; compatibility of deflection at B (delta_Bx = R_B f_BB with f_BB = L^3/3EI) gives R_B = x^2(3L-x)/2L^3. (Key point: Redundant and compatibility)

3. Which expression gives the hogging moment at A for a unit load at x?
   A. M_A = R_B L + x
   B. M_A = x - R_B L = x(L-x)(2L-x)/2L^2
   C. M_A = x(L-x)/L
   D. M_A = R_B x - L
   Answer: B. Taking moments about A for the cantilever: unit load gives x, the upward R_B gives R_B L, so M_A = x - R_B L. (Key point: Moment expression)

4. For L = 10 m, what is M_A for a unit load at mid-span, and the effect of a full-span UDL w?
   A. 1.875 hogging; M_A = wL^2/8 = 12.5w
   B. 1.875 hogging; M_A = wL^2/2 = 50w
   C. 2.5 hogging; M_A = 12.5w
   D. 0.3125 hogging; M_A = 12.5w
   Answer: A. At x = 5, R_B = 0.3125 and M_A = 5 - 3.125 = 1.875 (hogging); UDL times ILD area gives wL^2/8 = 12.5w. (Key point: Key ordinates and use)

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