A one-line estimate with a generic coefficient. Not a thermal stress analysis and not a design allowance. ΔL = α × L0 × ΔT assumes the coefficient is constant over the range, the material is isotropic, and nothing is holding the part. All three are usually false, and a constrained part does not expand, it loads. Open for the full scope limits.
What this tool actually does
Educational and estimation purposes only. This page produces a first-pass number, not a design figure.
Applies the linear thermal expansion formula to one dimension of one material over one temperature change, using a typical published coefficient of thermal expansion.
ΔL = α × L0 × ΔT
The model assumes a constant CTE across the whole temperature range, which is not always accurate, and it assumes the part is free to move.
Key factors not accounted for
- Non-linearity: CTE varies with temperature. Plastics change dramatically near the glass transition (Tg), and every material behaves differently near a melting point or other phase transition.
- Material variance: The listed values are generic and typical. Specific alloys, tempers, additives, fillers, reinforcements and processing methods all shift expansion behaviour, and the datasheet for the grade you actually bought governs.
- Anisotropy: many materials expand differently in different directions:
- Wood: radial against tangential against longitudinal grain
- Composites: along the fibres against across them
- 3D prints: layer adhesion direction effects
- Metals: rolling and extrusion direction effects
- Thermal hysteresis: some materials do not return to their original dimensions after temperature cycling.
- Constraint effects: a real assembly is usually restrained, so the temperature change produces stress rather than free movement. That stress is the number that breaks things, and this tool does not compute it.
- Moisture and environment: hygroscopic materials such as wood and several plastics expand and contract with humidity independently of temperature.
- Time-dependent effects: creep, stress relaxation and viscoelastic behaviour change dimensions over time under load and temperature.
Application-specific considerations
- Pressure vessels and piping: must follow the ASME Boiler and Pressure Vessel Code, ASME B31 piping codes, the applicable ASTM material standards and local regulations.
- Structural components: expansion joints, flexible connections and movement allowances require professional engineering analysis, not a single length change.
- Precision assemblies: tolerance stack-up must include thermal variation across the whole operating range, not the nominal condition.
- Dissimilar materials: bimetallic effects can generate significant stress at joints and interfaces even when each part is free on its own.
- Extreme temperatures: CTE at cryogenic or elevated temperatures can differ substantially from room-temperature data, which is what most published tables report.
Never use this as the design allowance for
- Pressure equipment, load-bearing structures, aerospace hardware or medical devices.
- Any case where the failure carries property damage, injury or a regulatory consequence.
- Complex geometries, or assemblies combining several materials.
- Environments outside normal atmospheric conditions.
- Anything requiring a certified calculation or a professional engineer's stamp.
Consult a qualified professional engineer for all of the above. Verify every value against the specific material datasheet and the applicable industry standard before it informs a tolerance, a gap or a joint.
A free length change, not a design allowance. The coefficient is a typical published value for a generic material, held constant across the range; a restrained part turns this movement into stress instead. Check the datasheet for the grade you are actually using, and get a professional engineer involved for pressure equipment, structures, precision assemblies and anything requiring a stamped calculation.
Coefficient of Thermal Expansion (CTE) values verified against authoritative datasheets and engineering references. Values are typical for materials at room temperature (20-25°C) and may vary with temperature, grade, and processing.
Primary Datasheet Sources
- MatWeb - Material property database with manufacturer datasheets
- Engineering Toolbox - Engineering materials reference database
- ASM Material Data Sheets - ASM International material specifications
- SpecialChem - Plastics material properties database
Comprehensive Material Reference Table
All materials in the calculator database with verified CTE sources.
| Material | CTE (µm/m·°C) | Source |
|---|---|---|
| METALS | ||
| Aluminum 3003 | 22.5-23.6 | Engineering Toolbox |
| Aluminum 6061 | 23.2-23.6 | MatWeb |
| Brass (Yellow) | 19.0-20.5 | Engineering Toolbox |
| Brass (Red) | 18.0-19.5 | Engineering Toolbox |
| Bronze (Commercial) | 17.5-18.5 | MatWeb (C93200) |
| Cast Iron, Gray | 10.5-11.2 | Engineering Toolbox |
| Cast Iron, Ductile | 11.0-12.0 | Engineering Toolbox |
| Copper (C10100/C11000) | 16.5-17.2 | MatWeb (C11000) |
| Gold | 14.0-14.3 | MatWeb: Elements |
| Lead | 28.0-30.0 | MatWeb: Elements |
| Magnesium | 25.0-26.5 | MatWeb: Elements |
| Nickel | 12.5-13.5 | MatWeb: Elements |
| Platinum | 8.8-9.2 | MatWeb: Elements |
| Silver | 18.5-19.7 | MatWeb: Elements |
| Steel, Carbon (1020) | 11.5-12.0 | MatWeb |
| Steel, Carbon (4140) | 11.5-13.0 | MatWeb |
| Steel, Stainless 304 | 17.2-17.3 | MatWeb |
| Steel, Stainless 316 | 15.5-16.5 | MatWeb |
| Steel, Tool A2 | 11.3-12.0 | Engineering Toolbox |
| Steel, Tool D2 | 10.2-10.8 | MatWeb |
| Titanium Grade 2 | 8.4-8.8 | Engineering Toolbox |
| Zinc | 29.0-31.0 | MatWeb: Elements |
| PLASTICS | ||
| ABS (Generic) | 75-95 | Professional Plastics |
| Acetal (POM) | 80-85 | Professional Plastics |
| Acrylic (PMMA) | 70-75 | Professional Plastics |
| CPVC | 69.5-80 | MatWeb (Corzan) |
| HDPE | 100-200 | MatWeb (Pipe) |
| LDPE | 100-240 | MatWeb (Sheet) |
| Nylon 6 | 70-85 | Professional Plastics |
| Nylon 6/6 | 70-85 | Professional Plastics |
| PEEK | 47-108 | MatWeb (450G) |
| Polybutylene (PB) | 120-140 | Engineering Toolbox |
| Polycarbonate (PC) | 65-70 | Professional Plastics |
| Polypropylene (PP) | 100-150 | Professional Plastics |
| Polystyrene (PS) | 65-75 | Professional Plastics |
| PET (Polyester) | 65-75 | Engineering Toolbox |
| PTFE (Teflon) | 100-165 | MatWeb |
| PVA | 80-90 | Engineering Toolbox |
| PVC (Rigid) | 75-85 | MatWeb (Piping) |
| PVDF | 100-200 | Technical Datasheet |
| WOOD (Anisotropic) | ||
| Fir (Parallel) | 3.5-4.2 | MST: Wood CTE |
| Fir (Perpendicular) | 28-38 | MST: Wood CTE |
| Oak (Parallel) | 4.5-5.5 | USDA Wood Handbook |
| Oak (Perpendicular) | 45-65 | Engineering Toolbox |
| Pine (Parallel) | 4.5-5.5 | Engineering Toolbox |
| Pine (Perpendicular) | 30-40 | Springer: J Wood Sci |
| CERAMICS & OTHERS | ||
| Alumina (99%) | 7.5-8.7 | Engineering Toolbox |
| Concrete | 10-14 | FHWA Research |
| Glass, Borosilicate | 3.25-3.3 | SCHOTT |
| Glass, Soda Lime | 8.5-9.5 | Engineering Toolbox |
| Quartz, Fused | 0.55-0.59 | Goodfellow |
General Reference Sources
Important Notes
- CTE values vary by temperature range - values shown are typically for 20-100°C
- Specific alloy grades may differ from generic material listings
- Fillers and reinforcements (e.g., glass fiber) significantly reduce CTE
- Wood is highly anisotropic - see WOOD section above for parallel vs perpendicular values
- Always consult manufacturer datasheets for critical applications
What is Linear Thermal Expansion?
Put simply: When things get hot, they get longer.
Notice in the animation above how the "Hot" atoms vibrate more aggressively? To maintain that movement without colliding, they push their neighbors further away (shown by the larger gaps).
Across billions of atoms, these microscopic gaps add up to a measurable change in length.
At the atomic level, heat is just energy. As a material gets warmer, its atoms vibrate more vigorously. This vibration creates "personal space" issues - the atoms push their neighbors slightly further away. Across billions of atoms, these microscopic pushes add up to a noticeable change in length. This is why bridges have "expansion joints" (gaps with teeth) and why power lines sag more on hot summer days.
Understanding the Formula
Engineers use a simple formula to estimate this growth:
ΔL = α · L₀ · ΔT
- ΔL (Delta L): The change in length (how much it grew).
- α (Alpha): The Coefficient of Thermal Expansion. This is a material property that says "how sensitive is this stuff to heat?"
- L₀: The original starting length.
- ΔT (Delta T): The change in temperature (Final - Initial).