---
title: "Deflection control, sufficient stiffness method"
subject: "Design of RCC Structure"
chapter: 8
key: "semester_7/design_of_rcc_structure:deflection-control-sufficient-stiffness-method"
source: https://www.bctengineer.com/q/semester_7/design_of_rcc_structure/deflection-control-sufficient-stiffness-method
site: BCT Engineering
---

# Deflection control, sufficient stiffness method

Design of RCC Structure · Chapter 8: Limit States of Serviceability: Deflection and Cracking

- Asked in: 2079 Baisakh, 4 marks; 2065 Shrawan (old course), 7 marks; 2065 Kartik (old course), 6 marks (asked 3 times)
- Video: [How to determine Modification factor as per IS:456-2000 ?](https://www.youtube.com/watch?v=ny7VEAuwM3s) — cwill structures
- Answer checked by Claude Opus 5.5 (high effort) on 2026-10-14
- Page: https://www.bctengineer.com/q/semester_7/design_of_rcc_structure/deflection-control-sufficient-stiffness-method
- Whole chapter: https://www.bctengineer.com/md/semester_7/design_of_rcc_structure/chapter-8

## Question

Explain how the deflection of an RC flexural member is controlled by the empirical (sufficient stiffness) method as per IS 456.

## Short answer

Deflection controlled by limiting span/effective depth ratio per IS 456 cl. 23.2.1. Basic l/d: cantilever 7, simply supported 20, continuous 26. Modified by factors kt (tension steel), kc (compression steel), kf (flanged beams). Permissible l/d = basic × kt × kc × kf. For spans >10m, basic value multiplied by 10/span. Actual l/d must not exceed permissible.

## Answer

#### Idea of the method
Calculating the actual deflection takes a long time, so IS 456 cl. 23.2.1 allows deflection to be controlled indirectly. If the ratio of span to effective depth of a beam, slab or cantilever does not exceed a permitted value, the deflection will be within the limits of cl. 23.2 (final deflection including creep, shrinkage and temperature $\le \text{span}/250$, and the part occurring after finishes are applied $\le \text{span}/350$ or 20 mm, whichever is less). This is the **empirical, or sufficient stiffness (span/depth ratio)**, method.

#### Procedure
1. Take the **basic span/effective depth ratio**:

| Member | Basic $l/d$ |
|---|---|
| Cantilever | 7 |
| Simply supported | 20 |
| Continuous | 26 |

2. Modify it by factors:
   - $k_t$: **modification factor for tension steel** from Fig. 4 of IS 456, which depends on $p_t$ and the service stress $f_s = 0.58 f_y \dfrac{A_{st,req}}{A_{st,prov}}$. Less steel and a lower stress give a larger factor (up to 2.0).
   - $k_c$: **modification factor for compression steel** from Fig. 5, based on $p_c = 100A_{sc}/bd$ (maximum 1.5).
   - $k_f$: **reduction factor for flanged beams** from Fig. 6, based on the ratio $b_w/b_f$ only (0.8 when $b_w/b_f \le 0.3$). For flanged beams, $p_t$ and $p_c$ for Figs. 4 and 5 are worked out on the area $b_f d$.
3. For spans above 10 m (other than cantilevers), the basic value is multiplied by $10/\text{span (m)}$; for cantilevers longer than 10 m, deflection must be calculated.
4. The **permissible ratio** is

$$
\left(\frac{l}{d}\right)_{perm} = \left(\frac{l}{d}\right)_{basic} \times k_t \times k_c \times k_f
$$

5. Compare it with the **actual** $l/d$. If actual $\le$ permissible, deflection is satisfied; if not, increase $d$ (or the steel) and check again.

#### Notes
- For two-way slabs, the check is made on the shorter span.
- This method is a conservative approximation of Annex C (the detailed method, which adds short-term, creep and shrinkage deflections).

## Check yourself

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

1. In the empirical method, deflection is controlled by
   A. Keeping span/effective depth within a permitted value
   B. Limiting bar diameter
   C. Calculating creep and shrinkage in full
   D. Limiting concrete cover
   Answer: A. If l/d is not more than permitted, deflection limits are satisfied. (Key point: Idea)

2. Basic l/d values for cantilever, simply supported and continuous members are
   A. 10, 20 and 30
   B. 26, 20 and 7
   C. 7, 20 and 26
   D. 20, 7 and 26
   Answer: C. IS 456 gives 7, 20 and 26 respectively. (Key point: Basic ratios)

3. The tension steel factor kt depends on
   A. The span only
   B. pt and service stress fs = 0.58 fy Ast,req/Ast,prov
   C. The bar diameter only
   D. fck only
   Answer: B. More steel and lower stress give a larger kt (up to 2.0). (Key point: Factor kt)

4. The permissible l/d is
   A. kt × kc only
   B. Basic l/d + kt + kc + kf
   C. Basic l/d × kt × kc × kf
   D. Basic l/d / kt
   Answer: C. Modification factors multiply the basic ratio; compare with the actual l/d. (Key point: Permissible ratio)

## Related in Design of RCC Structure

- [Crack control methods as per IS 456](https://www.bctengineer.com/question.md?key=semester_7%2Fdesign_of_rcc_structure%3Acrack-control-methods-as-per-is) — Design of RCC Structure, chapter 8
- [Load combinations for column per IS 456](https://www.bctengineer.com/question.md?key=semester_7%2Fdesign_of_rcc_structure%3Aload-combinations-for-column-per-is) — Design of RCC Structure, chapter 3
- [Deflection, crack width control, crack formula](https://www.bctengineer.com/question.md?key=semester_7%2Fdesign_of_rcc_structure%3Adeflection-crack-width-control-crack-formula) — Design of RCC Structure, chapter 8

## Related in other subjects

- [Stiffness matrix: frame, flexural deformations only](https://www.bctengineer.com/question.md?key=semester_5%2Ftheory_of_structures_ii%3Astiffness-frame-15knm-10kn-15knm-flexural) — Theory of Structures II, chapter 3
- [Stiffness method: frame, flexural deformations only](https://www.bctengineer.com/question.md?key=semester_5%2Ftheory_of_structures_ii%3Astiffness-frame-10kn-40knm-flexural) — Theory of Structures II, chapter 3
- [Stiffness matrix: element matrices, member forces, BMD](https://www.bctengineer.com/question.md?key=semester_5%2Ftheory_of_structures_ii%3Astiffness-element-matrices-600kn-bmd) — Theory of Structures II, chapter 3
- [Stiffness method: bent frame member end moments](https://www.bctengineer.com/question.md?key=semester_5%2Ftheory_of_structures_ii%3Astiffness-bent-frame-end-moments-inextensible) — Theory of Structures II, chapter 3
