RCC Beam / Footing Slab Design Calculator (LSM)
Beam Footing or Slab Design by Limit State Method
This article presents the design-check procedure, stress-block parameters, reinforcement calculation approach, and a numerical example for reinforced concrete beam or slab sections using the supplied design methodology.
Shear Design Flow Diagram
Procedure for Design Checks
For a given cross-section, the ultimate axial capacity is evaluated between the limiting strain conditions for pure compression and pure tension. For a specified bending moment, the corresponding ultimate axial force lies between these two limiting cases.
The neutral-axis depth $x$ is obtained by satisfying equilibrium between the internal forces and the factored axial force. It is determined from:
Where $N$ is the factored axial force, and $P_{us}(x)$ and $P_{uc}(x)$ represent the internal stress contributions from steel and concrete respectively:
Direct Solution for Rectangular Sections
The magnitude of compressive force $C_u$ and its location are determined from the compressive stress block. Ultimate structural failure occurs when the extreme compression fibre reaches the limiting strain $\epsilon_{cu}$.
Two distinct governing conditions are considered:
- Neutral axis lying within the section
- Neutral axis lying outside the section
1) Neutral Axis Within the Section
a) Parabolic-Rectangular Stress Block
When the neutral axis lies within the section depth, the extreme compression fibre reaches the limiting strain $\epsilon_{uc2}$. For a rectangular section of width $b$ and neutral-axis depth $x$, the resultant compression force is:
The centroid of $C_u$ from the extreme compression edge is located at $\beta_2 x$.
| Concrete Grade ($f_{ck}$) | $\beta_1$ | $\beta_2$ |
|---|---|---|
| $\le$ M40 | 0.80 | 0.42 |
| M45 | 0.79 | 0.42 |
| M50 | 0.78 | 0.42 |
| M55 | 0.77 | 0.42 |
| $\ge$ M60 | 0.76 | 0.42 |
| Parameter | $f_{ck}$ (N/mm²) | |||||
|---|---|---|---|---|---|---|
| $\le$ 60 | 70 | 75 | 90 | 100 | 115 | |
| $\beta_1$ | 0.8095 | 0.74194 | 0.69496 | 0.63719 | 0.59936 | 0.58333 |
| $\beta_2$ | 0.4160 | 0.39191 | 0.37723 | 0.36201 | 0.35294 | 0.35294 |
b) Simplified Rectangular Stress Block
A simplified rectangular stress block may be used in place of the parabolic-rectangular block. The corresponding parameters are defined as:
| Concrete Grade | $\lambda$ | $\eta$ |
|---|---|---|
| $\le$ M55 | 0.80 | 1.00 |
| M60 | 0.79 | 0.99 |
| M65 | 0.78 | 0.98 |
| M70 | 0.77 | 0.97 |
| M75 | 0.76 | 0.96 |
| M80 | 0.75 | 0.95 |
| $\ge$ M85 | 0.74 | 0.94 |
| Parameter | $f_{ck}$ (N/mm²) | |||||
|---|---|---|---|---|---|---|
| $\le$ 60 | 70 | 75 | 90 | 100 | 115 | |
| $\beta_1$ | 0.80 | 0.76781 | 0.73625 | 0.67500 | 0.61625 | 0.56000 |
| $\beta_2$ | 0.40 | 0.39375 | 0.38750 | 0.37500 | 0.36250 | 0.35000 |
2) Neutral Axis Outside the Section
a) Parabolic-Rectangular Stress Block
When the neutral axis lies outside the concrete section, the entire section remains in compression. The strain at the least-compressed edge is below the limiting value, while the maximum compression strain is taken as $\epsilon_{uc2}$.
The total compressive stress distribution comprises two parts:
- A full parabolic-rectangular profile over the depth corresponding to strain $\epsilon_{uc2}$.
- An additional parabolic portion over the remaining depth where strain transitions linearly from $\epsilon_{uc2}$ down to the minimum edge strain.
The resultant compression force $C_u$ and its line of action are obtained by superposition. The standard factors $\beta_1$ and $\beta_2$ are not directly applicable to this case; the appropriate integration relationships or codal tables should be used.
As defined in Clause 8.2.1 of the governing standards, intermediate strain distributions range between two limits:
- Uniform axial strain $\epsilon_{c2}$ across the entire section (pure compression).
- Strain varying from $\epsilon_{cu2}$ at the top edge to zero at the neutral axis position.
b) Rectangular Stress Block
For the external neutral-axis case, modified parameters $\lambda$, $\eta$, and $k$ are used with the simplified rectangular stress block.
| Concrete Grade ($f_{ck}$) | $\lambda$ | $\eta$ | $k$ |
|---|---|---|---|
| $\le$ M55 | 0.80 | 1.00 | 1.00 |
| M60 | 0.79 | 0.99 | 0.99 |
| M65 | 0.78 | 0.98 | 0.98 |
| M70 | 0.77 | 0.97 | 0.97 |
| M75 | 0.76 | 0.96 | 0.96 |
| M80 | 0.75 | 0.95 | 0.95 |
| $\ge$ M85 | 0.74 | 0.94 | 0.94 |
Note: Factor $k$ adjusts for effective stress block reduction under non-uniform compressive strain profiles.
| $f_{ck}$ (N/mm²) | $\lambda$ | $\eta$ | $k$ |
|---|---|---|---|
| $\le$ 60 | 0.8000 | 1.000 | 0.75000 |
| 70 | 0.7875 | 0.975 | 0.73016 |
| 75 | 0.7750 | 0.950 | 0.70968 |
| 90 | 0.7500 | 0.900 | 0.66667 |
| 100 | 0.7250 | 0.850 | 0.62069 |
| 115 | 0.7000 | 0.800 | 0.57143 |
| $x/h$ | $f_{ck} = 60$ N/mm² | $f_{ck} = 70$ N/mm² | $f_{ck} = 75$ N/mm² | $f_{ck} = 90$ N/mm² | $f_{ck} = 100$ N/mm² | $f_{ck} = 115$ N/mm² | ||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | |
| 1.0 | 0.80952 | 0.41597 | 0.74194 | 0.39191 | 0.69496 | 0.37723 | 0.63719 | 0.36201 | 0.59936 | 0.35482 | 0.58333 | 0.35294 |
| 1.2 | 0.89549 | 0.45832 | 0.83288 | 0.43765 | 0.78714 | 0.42436 | 0.72968 | 0.41022 | 0.69249 | 0.40355 | 0.67720 | 0.40186 |
| 1.4 | 0.93409 | 0.47480 | 0.88197 | 0.45841 | 0.84129 | 0.44724 | 0.78831 | 0.43492 | 0.75381 | 0.42907 | 0.73986 | 0.42761 |
| 1.6 | 0.95468 | 0.48304 | 0.91168 | 0.46990 | 0.87615 | 0.46046 | 0.82826 | 0.44975 | 0.79679 | 0.44461 | 0.78422 | 0.44335 |
| 1.8 | 0.96693 | 0.48779 | 0.93113 | 0.47702 | 0.90007 | 0.46895 | 0.85695 | 0.45954 | 0.82834 | 0.45499 | 0.81702 | 0.45389 |
| 2.0 | 0.97481 | 0.49077 | 0.94460 | 0.48178 | 0.91730 | 0.47478 | 0.87838 | 0.46644 | 0.85234 | 0.46237 | 0.84211 | 0.46140 |
| 2.5 | 0.98550 | 0.49475 | 0.96464 | 0.48861 | 0.94420 | 0.48347 | 0.91348 | 0.47705 | 0.89255 | 0.47385 | 0.88448 | 0.47311 |
| 5.0 | 0.99702 | 0.49893 | 0.99060 | 0.49705 | 0.98285 | 0.49512 | 0.96937 | 0.49234 | 0.95972 | 0.49089 | 0.95622 | 0.49057 |
| $x/h$ | $f_{ck} = 60$ N/mm² | $f_{ck} = 70$ N/mm² | $f_{ck} = 75$ N/mm² | $f_{ck} = 90$ N/mm² | $f_{ck} = 100$ N/mm² | $f_{ck} = 115$ N/mm² | ||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | $\beta_3$ | $\beta_4$ | |
| 1.0 | 0.80000 | 0.40000 | 0.76781 | 0.39375 | 0.73625 | 0.38750 | 0.67500 | 0.37500 | 0.61625 | 0.36250 | 0.56000 | 0.35000 |
| 1.2 | 0.88000 | 0.44000 | 0.85478 | 0.43750 | 0.82500 | 0.43125 | 0.76000 | 0.42000 | 0.69500 | 0.40625 | 0.63200 | 0.39250 |
| 1.4 | 0.91429 | 0.45714 | 0.89048 | 0.45625 | 0.86321 | 0.45089 | 0.80000 | 0.44000 | 0.73571 | 0.42589 | 0.67143 | 0.41429 |
| 1.6 | 0.93750 | 0.46875 | 0.91563 | 0.46875 | 0.89063 | 0.46563 | 0.82813 | 0.45313 | 0.76563 | 0.44063 | 0.70000 | 0.43125 |
| 1.8 | 0.95556 | 0.47778 | 0.93542 | 0.47813 | 0.91250 | 0.47656 | 0.85000 | 0.46250 | 0.78889 | 0.45156 | 0.72222 | 0.44444 |
| 2.0 | 0.97000 | 0.48500 | 0.95100 | 0.48563 | 0.93000 | 0.48500 | 0.86750 | 0.47000 | 0.80750 | 0.46063 | 0.74000 | 0.45500 |
| 2.5 | 0.98400 | 0.49200 | 0.96880 | 0.49375 | 0.95200 | 0.49500 | 0.89200 | 0.48000 | 0.83200 | 0.47250 | 0.76800 | 0.47000 |
| 5.0 | 0.99600 | 0.49800 | 0.99040 | 0.49875 | 0.98400 | 0.50000 | 0.93600 | 0.49000 | 0.88800 | 0.48500 | 0.84000 | 0.48500 |
Note: The design tables above are sourced from standard IRC guidelines.
Estimation of Required Steel Area ($A_{st}$)
Numerical Example
Given Parameters: Ultimate moment $M_u = 150\text{ kNm}$, Effective cover $= 50\text{ mm}$, Concrete Grade M45, Provided total depth $D = 250\text{ mm}$, Bar diameter $\phi = 20\text{ mm}$.
Required $D \approx 142.2 + 10\text{ (bar radius)} + 50\text{ (cover)} = 202.2\text{ mm} < 250\text{ mm}$.
Result: Provided overall depth is adequate.
Effective depth $d = 250 - 50 - 10 = 190\text{ mm}$.
Since $x/d = 0.290 < 0.617$ (limiting value), the tensile steel yields, confirming an under-reinforced section.
Insight: An increase of $47\text{ mm}$ in section depth significantly reduces $x/d$ from $0.617$ (balanced condition) down to $0.290$.
If a balanced section lever arm is incorrectly assumed, steel area calculation yields:
Assuming a balanced lever arm causes roughly an 18% over-estimation of reinforcement. The neutral axis depth shifts from $117.23\text{ mm}$ to $55.1\text{ mm}$, shifting $x/d$ from $0.617$ down to $0.290$.
Conclusion: When actual provided depth exceeds the minimum required depth, always compute the true neutral axis position rather than assuming balanced conditions to avoid unnecessary over-reinforcement.
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