IS 8147

: 1976

Code of Practice for the use of Aluminium Alloys in Structures

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This code of practice provides guidelines for the structural use of aluminium alloys based on the Working Stress Method (WSM). It covers material specifications, general design requirements, design of members under various loads (tension, compression, bending), and provisions for connections, fabrication, and erection.

Code of Practice for the use of Aluminium Alloys in Structures

Quick Reference Values
Modulus of Elasticity, E0.7 x 10^5 N/mm²
Poisson's Ratio, v0.33
Modulus of Rigidity, G0.26 x 10^5 N/mm²
Coefficient of Linear Thermal Expansion23 x 10^-6 per °C
Unit Mass of Aluminium2700 kg/m³
Factor of Safety on Ultimate Stress (Tension)1.95
Key Formulas
Pc = 125 - 0.75 * (l/r) — Permissible compressive stress for Alloy H20-WP (6351S-T6) for l/r < 67
Practical Notes
This 1976 version uses the Working Stress Method (WSM). It has been superseded by IS 8147:2023, which adopts the Limit State Method (LSM), making the design philosophy consistent with modern steel (IS 800) and concrete (IS 456) codes.
Aluminium's Modulus of Elasticity is approximately one-third that of steel, resulting in larger deflections. Serviceability and deflection checks are critical.
The mechanical properties of aluminium are highly dependent on the alloy and its temper condition (e.g., 6061-T6). Careful selection based on Table 1 is essential.