SUMMARY
To maintain an aluminum bar's length at 15°C when the temperature increases to 35°C, a stress of 16.52 GPa is required. This calculation utilizes Young's modulus (70 GPa) and the coefficient of thermal expansion (23.6 x 10^-6 m/m°C) for aluminum. The formula used is Stress = Young's modulus x Coefficient of thermal expansion x Change in temperature. Understanding these principles allows for precise calculations of thermal stress in materials.
PREREQUISITES
- Young's modulus for aluminum (70 GPa)
- Coefficient of thermal expansion for aluminum (23.6 x 10^-6 m/m°C)
- Basic principles of thermal expansion
- Understanding of kinetic theory of matter
NEXT STEPS
- Research the properties of aluminum, focusing on Young's modulus and thermal expansion coefficients.
- Learn how to apply the formula for thermal stress in different materials.
- Explore the effects of temperature changes on material properties in engineering applications.
- Investigate real-world applications of thermal stress calculations in structural engineering.
USEFUL FOR
Engineers, materials scientists, and students studying thermodynamics or materials science will benefit from this discussion, particularly those focused on thermal stress and material properties.