Thermal Stress Calculator
Enter Young's modulus E, expansion coefficient α and temperature change ΔT to compute thermal stress σ=E·α·ΔT. E=200 GPa, α=12e-6/K, ΔT=50 K → σ=120 MPa, ΔL=6e-4 m.
Input Data
Results
At a glance:Thermal stress is the internal mechanical stress a solid develops from a temperature change. When temperature changes, its length would freely expand/contract by ΔL_free=α·L·ΔT (α linear expansion coefficient, L original length, ΔT temperature change). If the ends are constrained (fixed supports, rigid connection) and cannot move freely, an opposite strain builds inside, producing thermal stress σ=E·α·ΔT (E Young's modulus). Direction: heating while blocked → compressive stress; cooling while blocked → tensile stress. The thermal strain ε=α·ΔT is the free strain from temperature; when constrained it becomes elastic strain ε_el=σ/E, and compatibility gives α·ΔT+σ/E=0 → σ=−E·α·ΔT (sign convention). This tool outputs the magnitude σ=E·α·ΔT. α meaning: elongation per unit length per 1 K. Common α (1/K): Invar 1.2e-6 (watches, gauges, very stable), glass 9e-6, concrete 10e-6, steel 12e-6, copper 17e-6, brass 19e-6, aluminium 23e-6, zinc 30e-6, plastics 50–100e-6. High-α materials are temperature-sensitive (aluminium expands ~2× steel). Typical stress: steel ΔT=50 K → σ=200GPa×12e-6×50=120 MPa (half of 250 MPa yield, not negligible); concrete ΔT=30 K → σ=30GPa×10e-6×30=9 MPa (near its 3–5 MPa tensile strength, so it cracks). History: 18th-century temperature compensation in compasses/watches, 19th-century rail buckling, 20th-century jet-engine thermal-stress analysis. Applications: bridge expansion joints; rail welding and track stability; engine piston/cylinder clearances; toughened glass; electronic packaging fatigue (different α of chip/mold/substrate); building expansion joints every 30–50 m; bimetallic strips (thermostats); quench cracking. Notes: (1) assumes fully constrained ends — partial restraint reduces stress; (2) assumes uniform temperature — gradients add bending stress; (3) beyond elastic limit needs elastoplastic analysis; (4) α, E vary with temperature (integrate at high T); (5) composites need compatibility + equilibrium.
Formula
Thermal stress: σ = E·α·ΔT (fully constrained)
Thermal strain: ε = α·ΔT
Free expansion: ΔL = α·L·ΔT
Compatibility: α·ΔT + σ/E = 0 → σ = −E·α·ΔT
Fully free member: σ = 0
$$\sigma = E\,\alpha\,\Delta T, \quad \varepsilon = \alpha\,\Delta T, \quad \Delta L = \alpha\,L\,\Delta T$$How to Use
- Enter Young's modulus E (Pa) and expansion coefficient α (1/K).
- Enter temperature change ΔT (K) and member length L (m).
- The tool shows σ (Pa, MPa), free expansion ΔL and strain ε.
Case Studies
Bridge joints and rails
A long steel bridge ΔT=50 K → σ=120 MPa; without expansion joints it would buckle.
Joints every span let it expand freely, avoiding the 120 MPa stress.
Welded rails must account for temperature swings and lateral stability (buckling).
Content review: Calculatorism Science Team. Results are for reference only; please refer to the relevant authorities for the official figures.