IS 11504-1985 provides comprehensive criteria for the structural design of reinforced concrete natural draught cooling towers, primarily focusing on hyperbolic shell structures. It covers analysis methods, load considerations including wind, earthquake, and thermal effects, reinforcement detailing, foundation design, and construction tolerances. This standard is essential for civil and structural engineers involved in designing and constructing durable, safe, and efficient cooling towers used in thermal power plants and heavy industries.
Overview
IS 11504-1985 provides comprehensive criteria for the structural design of reinforced concrete natural draught cooling towers, primarily focusing on hyperbolic shell structures. It covers analysis methods, load considerations including wind, earthquake, and thermal effects, reinforcement detailing, foundation design, and construction tolerances. This standard is essential for civil and structural engineers involved in designing and constructing durable, safe, and efficient cooling towers used in thermal power plants and heavy industries.
Audience
Contents
Structure
IS 11504: Scope - Key Symbols, Proportions & Construction Checks
Geometry & Dimensions:
Material Properties:
Stress Resultants:
Loads & Pressures:
| Height Range | Allowable Survey Inaccuracy |
|---|---|
| Up to 30 m | ± 15 mm |
| 30 to 60 m | ± 40 mm |
| 60 to 120 m | ± 60 mm |
| Above 120 m | ± 80 mm |
graph TD
A[Shell Geometry] -->|Dimensions| B(Base Diameter D)
A --> C(Height H)
A --> D(
IS 11504 - Key Definitions, Symbols & Wind Pressure Distribution
| Symbol | Meaning |
|---|---|
| Tth | Throat radius |
| D | Base diameter at basin sill level |
| E | Modulus of elasticity of concrete (short-term) |
| Fa | Fourier coefficient of nth term |
| ₫ | Thickness of the shell |
| H | Total tower height above basin sill level |
| Hm | Meridional moment/unit length of middle surface |
| M | Circumferential moment/unit length of middle surface |
| M₁, M₂ | Twisting moments/unit length of middle surface |
| N₁ | Meridional stress resultant/unit length of middle surface |
| N₂ | Circumferential stress resultant/unit length of middle surface |
| Nu, Ne | Shearing stress resultants/unit length of middle surface |
| p' | Design wind pressure coefficient |
| Pcr | Critical buckling pressure |
| Ro | Horizontal radius |
| Hb | Vertical distance from throat to basin sill level |
| rt | Top radius |
| ν | Poisson's ratio of concrete |
The wind pressure coefficient around the shell is:
[ p'(\theta) = \sum_{n=0}^7 F_n \cos(n \theta) ]
| n | (F_n) |
|---|---|
| 0 | -0.00071 |
| 1 | +0.24611 |
| 2 | +0.62296 |
| 3 | +0.48833 |
| 4 | +0.10756 |
| 5 | -0.09579 |
| 6 | -0.01142 |
| 7 | +0.04551 |
This series is accurate up to 7 terms.
IS 11504 - Symbols, Notations & Key Formulas
| Symbol | Meaning |
|---|---|
| Tth | Throat radius |
| D | Base diameter at basin sill level |
| E | Modulus of elasticity of concrete (short term) |
| Fa | Fourier coefficient of nth term |
| ₫ | Thickness of the shell |
| H | Total tower height above basin sill level |
| Mₘ | Meridional moment per unit length |
| Mₙ | Circumferential moment per unit length |
| Nₘ | Meridional stress resultant per unit length |
| Nₙ | Circumferential stress resultant per unit length |
| p' | Design wind pressure coefficient |
| Pcr | Critical buckling pressure |
| Ro | Horizontal radius |
| Hb | Vertical distance from throat to basin sill |
| rt | Top radius |
| ν | Poisson's ratio of concrete |
[ p'(\theta) = \sum_{n=0}^{7} F_n \cos(n\theta) ]
| n | (F_n) |
|---|---|
| 0 | -0.00071 |
| 1 | +0.24611 |
| 2 | +0.62296 |
| 3 | +0.48833 |
| 4 | +0.10756 |
| 5 | -0.09579 |
| 6 | -0.01142 |
| 7 | +0.04551 |
Use with basic wind pressure from IS 875.
[ \frac{r^2}{a^2} - \frac{y^2}{b^2} = 1 ]
[ R_m = r \csc \phi = \frac{r(1 + (dr/dy)^
IS 11504: Key Formulas, Tables & Specifications for Materials
| Symbol | Meaning |
|---|---|
| Tth | Throat radius |
| D | Base diameter at basin sill |
| E | Modulus of elasticity of concrete |
| ν | Poisson's ratio of concrete |
| M, N | Moment and stress resultants |
| p' | Design wind pressure coefficient |
[ \text{Dead Load} = \text{Unit weight} \times \text{Volume} ]
| Grade | Yield Strength (f_y) (MPa) | Typical Use |
|---|---|---|
| Fe 415 | 415 | Mild steel reinforcement |
| Fe 500 | 500 | High strength deformed bars |
| Fe 550 | 550 | Higher strength bars |
flowchart TD
A[Materials] --> B[Concrete
IS 11504: Loads and Load Combinations
| Load Combination No. | Load Combination Formula |
|---|---|
| 1 | 1.5 × Dead Load (DL) |
| 2 | 1.2 × DL + 1.6 × Live Load (LL) + 0.5 × Earthquake Load (EL) |
| 3 | 1.2 × DL + 1.6 × EL + 0.5 × LL |
| 4 | 0.9 × DL + 1.6 × EL |
flowchart LR
DL[Dead Load] --> LC[Load Combination]
LL[Live Load] --> LC
EL[Earthquake Load] --> LC
TRL[Thermal Restraint Load] --> LC
CL[Construction Load] --> LC
OL[Other Loads] --> LC
LC --> Design[Design Load for Analysis]
For detailed values and factors, refer to IS 875 (Part 5) and IS 1911 for dead load assessment.
IS 11504 - Tower Design Considerations: Key Points
| Tower Height | Foundation Type |
|---|---|
| > 75 m | Continuous foundation or annular pile cap |
| ≤ 75 m | Individual isolated foundations |
graph TD
A[Tower Height] -->|> 75 m| B[Continuous Foundation]
A -->|≤ 75 m| C[Isolated Foundation]
D[Vibration Frequency] -->|Inversely proportional| E[Tower Height & Mass]
E --> F[Design for Wind-Induced Vibrations]
Summary: Use IS 456 for stresses, design foundations based on height, and carefully assess vibration for tall towers to ensure structural safety.
IS 11504: Constructional Aspects - Key Formulas, Tables & Specifications
| Parameter | Tolerance |
|---|---|
| Shell wall centre line (horizontal plane, 3m chord) | ±15 mm |
| Shell wall centre line (meridional plane, 1m height) | ±10 mm |
| Shell thickness | +10 mm / -5 mm |
| Horizontal radius (any section except base) | ±50 mm |
| Horizontal radius (shell base) | ±40 mm |
| Height Range | Allowance for Survey Inaccuracy |
|---|---|
| Up to 30 m | ±15 mm |
| 30 m to 60 m | ±40 mm |
| 60 m to 120 m | ±60 mm |
| Above 120 m | ±80 mm |
graph TD
A[Shell Construction] --> B[Dimensional Tolerances]
B --> C[Horizontal Centre Line ±15 mm]
B --> D[Meridional Centre Line ±10 mm]
B --> E[Thickness +10/-5 mm]
B --> F[Horizontal Radius ±40 to 50 mm]
A --> G[Geometry Checks]
G --> H[Ground Stations ≤10° apart]
G --> I[Height-based survey inaccuracies]
I --> J[≤30m: ±15 mm]
I --> K[30-60m: ±40 mm]
I --> L[60-120m: ±
Wind Pressure Distribution on Cooling Tower Shell (IS 11504 - Appendix A)
[ p'(\theta) = \sum_{n=0}^{7} F_n \cos(n \theta) ]
| n | (F_n) |
|---|---|
| 0 | -0.00071 |
| 1 | +0.24611 |
| 2 | +0.62296 |
| 3 | +0.48833 |
| 4 | +0.10756 |
| 5 | -0.09579 |
| 6 | -0.01142 |
| 7 | +0.04551 |
Series up to 7 terms provides sufficient accuracy.
[ p_{design}(\theta) = p_{basic} \times p'(\theta) ]
graph LR
A[Basic Wind Pressure (IS 875)] --> B[Multiply by p'(\u03B8)]
B --> C[Design Wind Pressure Distribution]
C --> D[Shell Surface Load]
This method ensures accurate circumferential wind load modeling for cooling tower shell design.
IS 11504 - Analysis of Shell (Clause 6.3.1 & Appendix B)
| Symbol | Meaning |
|---|---|
| Tth | Throat radius |
| D | Base diameter at basin sill level |
| E | Modulus of elasticity of concrete |
| t | Thickness of shell |
| H | Total tower height above basin sill |
| Mθ, Mφ | Meridional and circumferential moments |
| Nθ, Nφ | Meridional and circumferential stress resultants |
| Qθ, Qφ | Transverse shear stress resultants |
| ν | Poisson's ratio of concrete |
[ \frac{dN_\theta}{d\theta} + (N_\phi - N_\theta) \cot \theta + q R = 0 ]
graph LR
A[Shell of Revolution] --> B[Membrane Analysis]
A --> C[Bending Analysis (Recommended)]
B --> D[Stress Resultants Nθ, Nφ]
C --> E[Moments Mθ, Mφ and Shear Qθ, Qφ]
F[Boundary Conditions] --> G[Upper Edge: Free, Smooth Transition]
F --> H[Lower Edge: Elastic Support, Thickened Ring Beam]
For detailed formulas and equilibrium equations, refer to Appendix B of IS 11504.
Frequently Asked
According to IS 11504 (1985) for reinforced concrete natural draught cooling towers, the structural design must consider the following types of loads:
| Load Type | Description |
|---|---|
| Dead Load | Self-weight of structure |
| Wind Load | Static + dynamic effects |
| Thermal Load | Temperature gradients |
| Seismic Load | Earthquake forces (zone dependent) |
| Hydrostatic Load | Water pressure inside or outside shell |
| Construction/Other | Temporary or imposed loads |
Loading diagram...
Designers should ensure all these loads are combined per relevant IS codes and analyzed using thin shell theory as recommended.
Minimum Reinforcement and Spacing for Cooling Tower Shells (IS 11504: Clause 6.3.6)
Minimum reinforcement ratio:
Maximum spacing:
Layering:
| Parameter | Value |
|---|---|
| Min. reinforcement (mild steel) | 0.35% of gross cross-sectional area |
| Min. reinforcement (high strength bars) | 0.25% of gross cross-sectional area |
| Max. spacing | 2 × shell thickness |
| Reinforcement layers | 2 layers if thickness ≥ 175 mm |
This ensures adequate crack control and structural integrity under thermal and wind loads typical for natural draught cooling towers.
Loading diagram...
IS 11504 on Wind Pressure Distribution & Aerodynamic Effects on Cooling Towers
| n | (F_n) |
|---|---|
| 0 | -0.00071 |
| 1 | +0.24611 |
| 2 | +0.62296 |
| 3 | +0.48833 |
| 4 | +0.10756 |
| 5 | -0.09579 |
| 6 | -0.01142 |
| 7 | +0.04551 |
Loading diagram...
This approach captures aerodynamic effects and pressure variation circumferentially on the cooling tower shell.
IS 11504 Construction Tolerances for Shell Geometry and Thickness
Survey Accuracy Allowances for Horizontal Radius Checks (Clause 7.4):
| Height Range (m) | Allowance (mm) |
|---|---|
| Up to 30 | ±15 |
| 30 to 60 | ±40 |
| 60 to 120 | ±60 |
| Above 120 | ±80 |
Key Notes:
Loading diagram...
These tolerances ensure dimensional accuracy critical for shell stability and performance.
To minimize stress concentrations around openings and fixtures in shells per IS 11504 Clause 6.3.5:
Summary Table for Reinforcement at Openings:
| Location | Reinforcement Area |
|---|---|
| Edges | ≥ 75% of intercepted reinforcement |
| Corners (diagonal) | 0.5 × shell thickness (d) in cm² |
This approach ensures smooth load transfer and reduces local stress peaks, enhancing shell durability.
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