| Thermal conductivity of pure aluminium | Approximately 237 W/m·K at 20°C | Provides a reference point for aluminium’s high heat-spreading capability. | Use high-purity aluminium where maximum thermal conduction is more important than strength or corrosion resistance. |
| Thermal conductivity of 6061 aluminium | Approximately 167 W/m·K at 20°C | Offers a useful balance between conductivity, strength, machinability and corrosion resistance. | Suitable for machined heat sinks, cold plates, structural thermal parts and general-purpose enclosures. |
| Thermal conductivity of 6063 aluminium | Approximately 201 W/m·K at 20°C | Higher conductivity than 6061 and excellent extrusion performance support efficient fin profiles. | Use for extruded heat sinks when fin density, surface finish and thermal performance are important. |
| Thermal conductivity of die-cast aluminium | Typically about 90–120 W/m·K, depending on alloy and casting quality | Lower conductivity and internal porosity can limit heat spreading compared with wrought aluminium. | Keep heat paths short, avoid excessive wall thickness and specify suitable alloy and casting quality for thermal areas. |
| Natural-convection heat-transfer coefficient | Approximately 5–25 W/m²·K in still or mildly moving air | Natural convection is quiet but generally removes heat more slowly than forced airflow. | Increase exposed surface area, orient vertical fins upward and provide unobstructed air gaps. |
| Forced-air heat-transfer coefficient | Approximately 25–100 W/m²·K for typical forced-air cooling | Air movement reduces the thermal boundary layer and substantially improves heat rejection. | Use fans or controlled airflow, while considering pressure drop, noise, dust and fan reliability. |
| Liquid-cooling heat-transfer coefficient | Approximately 500–10,000 W/m²·K, depending on fluid, velocity and flow regime | Liquid cooling can remove substantially more heat per unit area than air cooling. | Use a low-resistance cold plate, sufficient flow velocity and compatible materials to control corrosion risk. |
| Thermal interface material thickness | Commonly about 0.05–0.20 mm for a well-controlled interface | Interface resistance can dominate total thermal resistance when the contact layer is thick or uneven. | Minimize bond-line thickness, maintain uniform pressure and select a material with suitable thermal conductivity. |
| Typical thermal conductivity of thermal interface materials | Approximately 1–15 W/m·K for many commercial pads, greases and phase-change materials | Even a thermally conductive interface is far less conductive than aluminium. | Prioritize thinness and complete surface coverage rather than relying only on a high conductivity rating. |
| Surface emissivity | Polished aluminium: approximately 0.03–0.10; anodized aluminium: approximately 0.70–0.90 | Higher emissivity improves radiative heat transfer, especially when airflow is limited. | Use a suitably anodized or coated surface when radiation is a meaningful part of the cooling strategy. |
| Radiative heat transfer | Strongly affected by emissivity, absolute temperature and view factor | Radiation becomes more useful as component temperature rises and surrounding surfaces allow heat exchange. | Keep high-emissivity surfaces exposed and avoid enclosing the heat sink in reflective, poorly ventilated spaces. |
| Fin spacing for natural convection | Often approximately 6–12 mm for vertical plate fins; final spacing depends on height and heat load | Fins that are too close restrict buoyancy-driven airflow and reduce effective cooling area. | Optimize fin spacing with thermal simulation or testing; do not maximize fin count without checking airflow. |
| Fin spacing for forced convection | Often approximately 2–6 mm, depending on fan capacity, fin height and pressure drop | Forced airflow permits denser fins, but excessive density increases resistance and can reduce actual airflow. | Match fin pitch to the fan’s pressure-flow curve and keep air paths clean and straight. |
| Thermal expansion of aluminium | Approximately 23 × 10⁻⁶ /K for common aluminium alloys | Temperature changes can create mechanical stress, joint movement and contact-pressure variation. | Allow for expansion in mounts, use compatible materials and avoid excessive clamping stress. |
| Thermal resistance calculation | Rθ = ΔT / Q; lower Rθ means better cooling | Thermal resistance links heat load and temperature rise in a measurable design target. | Evaluate the complete path: source-to-interface, interface-to-spreader, spreader-to-air or liquid and ambient conditions. |
| Surface flatness and contact quality | Lower roughness, better flatness and uniform clamping generally reduce contact resistance | Air gaps are highly insulating compared with aluminium and can sharply increase junction temperature. | Machine critical contact surfaces, remove burrs and apply controlled mounting pressure across the full contact area. |
| Material thickness and heat spreading | Thicker bases improve spreading up to a point; excessive thickness adds mass and cost | A thin base may create local hot spots before heat reaches the fins or cooling channels. | Size the base for the heat-source footprint, heat flux and allowable temperature difference rather than thickness alone. |
| Airflow cleanliness | Dust and debris can progressively reduce open area and increase thermal resistance | Contamination blocks channels and acts as an insulating layer on fin surfaces. | Provide filtration, service access and sufficient fin spacing for the expected operating environment. |