---
title: "Symmetrical I-beam: moment, flange and web share"
subject: "Strength of Materials"
chapter: 7
key: "semester_3/strength_of_materials:symmetrical-i-beam-max-moment-flange"
source: https://www.bctengineer.com/q/semester_3/strength_of_materials/symmetrical-i-beam-max-moment-flange
site: BCT Engineering
---

# Symmetrical I-beam: moment, flange and web share

Strength of Materials · Chapter 7: Theory of Flexure

- Asked in: 2066 Bhadra (old course), 10 marks
- Video: [Shape Factor Problem No 1 ( Symmetrical I  Section )](https://www.youtube.com/watch?v=Yemto1mozKU) — Stan Academy
- Answer checked by Claude Opus 5.5 (high effort) on 2026-10-14
- Page: https://www.bctengineer.com/q/semester_3/strength_of_materials/symmetrical-i-beam-max-moment-flange
- Whole chapter: https://www.bctengineer.com/md/semester_3/strength_of_materials/chapter-7

## Question

An I section beam (symmetrical) has 200mm wide flanges and overall depth 500mm. Each flange is 25mm thick and the web is 20mm thick. Determine (i) the maximum bending moment that should be imposed in the section if the tensile or the compressive stress is not to exceed $40\ \text{N/mm}^2$ (ii) What percentage of the moment is resisted by flanges and web?

## Short answer

Maximum bending moment is 114.63 kNm. The flanges resist 78.8% of the moment and the web 21.2%.

## Answer

**Given:** flanges 200 mm × 25 mm, overall depth 500 mm, web 20 mm thick (web depth $500 - 50 = 450$ mm). $\sigma_{max} = 40\ \text{N/mm}^2$.

```text
 +-----------+  25
     | |
     | |       450
 +-----------+  25
     200 wide, web 20
```

#### Moment of inertia
$$
I = \frac{200\times500^3 - 180\times450^3}{12} = 7.1646\times10^8\ \text{mm}^4
$$

#### (i) Maximum bending moment
Extreme fibre distance $y = 250$ mm:

$$
M = \frac{\sigma I}{y} = \frac{40\times7.1646\times10^8}{250} = 114.63\times10^6\ \text{Nmm} = 114.63\ \text{kNm}
$$

#### (ii) Moment shared by flanges and web
Stress at distance $y$ is $\sigma = 40y/250$.

Flanges (both, from $y = 225$ to $250$):

$$
M_f = 2\int_{225}^{250}\frac{40y}{250}\,200\,y\,dy = 2\times\frac{40\times200}{250}\times\frac{250^3 - 225^3}{3} = 90.33\ \text{kNm}
$$

Web (from $-225$ to $225$):

$$
M_w = \frac{40\times20}{250}\times\frac{2\times225^3}{3} = 24.30\ \text{kNm}
$$

Check: $90.33 + 24.30 = 114.63$ kNm.

| Part | Moment (kNm) | Share |
|---|---|---|
| Flanges | 90.33 | 78.8% |
| Web | 24.30 | 21.2% |

**Answer: (i) $M_{max} = 114.63$ kNm; (ii) flanges carry 78.8% and the web 21.2% of the moment.**

## Check yourself

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

1. How is I of the I section found?
   A. I = 200x500^3/12
   B. I = [200x500^3 - 200x450^3]/12
   C. I = [200x500^3 - 180x450^3]/12 (outer rectangle minus voids)
   D. I = 20x450^3/12 only
   Answer: C. The voids on each side of the web are 90 mm wide each, 180 mm total, 450 mm deep. (Key point: Moment of inertia)

2. Which relation gives the allowable moment?
   A. M = sigma I/y with y = 225 mm
   B. M = sigma A y
   C. M = sigma y/I
   D. M = sigma I/y with y = 250 mm, giving 114.63 kNm
   Answer: D. The limiting stress occurs at the extreme fibre, 250 mm from the NA. (Key point: Maximum moment)

3. How does bending stress vary through the section?
   A. Linearly with distance from the NA, sigma = 40y/250
   B. Uniformly over the flange
   C. Parabolically
   D. Maximum at the NA
   Answer: A. Bending stress is proportional to y. (Key point: Stress distribution)

4. What share of the moment do the flanges carry?
   A. About 21.2%
   B. About 78.8% (90.33 kNm)
   C. About 50%
   D. About 95%
   Answer: B. Flanges are far from the NA, so they carry the greater part; the web carries 24.30 kNm, 21.2%. (Key point: Flange share)

## Related in Strength of Materials

- [Bending stress diagram; moment in flanges](https://www.bctengineer.com/question.md?key=semester_3%2Fstrength_of_materials%3Al-section-bending-stress-diagram-flange) — Strength of Materials, chapter 7
- [T-beam: maximum tensile and compressive stress](https://www.bctengineer.com/question.md?key=semester_3%2Fstrength_of_materials%3At-beam-udl-40kn-30cm-tension) — Strength of Materials, chapter 7
- [I-section beam: moment of resistance and UDL](https://www.bctengineer.com/question.md?key=semester_3%2Fstrength_of_materials%3Ai-section-moment-resistance-udl-10m) — Strength of Materials, chapter 7
- [Simply supported I-beam: stress at flange-web junction](https://www.bctengineer.com/question.md?key=semester_3%2Fstrength_of_materials%3Ai-beam-flange-web-junction-stress) — Strength of Materials, chapter 7
- [T-beam: bending stress 15 cm above base](https://www.bctengineer.com/question.md?key=semester_3%2Fstrength_of_materials%3At-beam-udl-5m-bending-stress) — Strength of Materials, chapter 7
- [Cantilever 5 m: maximum and 25 mm bending stress](https://www.bctengineer.com/question.md?key=semester_3%2Fstrength_of_materials%3Acantilever-5m-8kn-15kn-bending-stresses) — Strength of Materials, chapter 7

## Related in other subjects

- [Bending stresses in a T-section beam](https://www.bctengineer.com/question.md?key=semester_4%2Fstrength_of_materials_mechanical%3Acast-iron-t-beam-bending-stresses) — Strength of Materials, chapter 3
- [Principal stresses at web-flange junction](https://www.bctengineer.com/question.md?key=semester_4%2Fstrength_of_materials_mechanical%3Aprincipal-stresses-web-flange-junction) — Strength of Materials, chapter 9
- [Ultimate moment of T-beam (2250 mm flange)](https://www.bctengineer.com/question.md?key=semester_7%2Fdesign_of_rcc_structure%3Aultimate-moment-of-t-beam-2250) — Design of RCC Structure, chapter 4
- [L-beam reinforcement for given moment](https://www.bctengineer.com/question.md?key=semester_7%2Fdesign_of_rcc_structure%3Al-beam-reinforcement-for-given-moment) — Design of RCC Structure, chapter 4
