Air Properties Table (1 atm)
Temperature-dependent thermophysical properties of dry air: density, cp, viscosity, thermal conductivity, Prandtl number. 200K–2000K. Sortable.
This free online air properties table (1 atm) provides instant results with no signup required. All calculations run directly in your browser — your data is never sent to a server. Supports both metric (SI) and imperial units with built-in unit selection dropdowns on every input field, so you can work in whatever units your problem provides. Designed for engineering students and professionals working through coursework, design projects, or quick reference calculations.
Air Properties Table (1 atm)
Temperature-dependent thermophysical properties of dry air at atmospheric pressure. Click column headers to sort.
42 rows shown
| T (K) ↑ | T (°C) | ρ (kg/m³) | cp (kJ/kg·K) | μ×10⁻⁵ (kg/m·s) | ν×10⁻⁶ (m²/s) | k×10⁻³ (W/m·K) | Pr | α×10⁻⁵ (m²/s) |
|---|---|---|---|---|---|---|---|---|
| 200 | -73 | 1.7458 | 1.007 | 1.329 | 7.61 | 18.1 | 0.737 | 1.033 |
| 220 | -53 | 1.5874 | 1.007 | 1.453 | 9.148 | 19.89 | 0.728 | 1.123 |
| 240 | -33 | 1.4533 | 1.007 | 1.574 | 10.83 | 21.55 | 0.721 | 1.235 |
| 250 | -23 | 1.3947 | 1.006 | 1.632 | 11.7 | 22.3 | 0.716 | 1.288 |
| 260 | -13 | 1.3416 | 1.006 | 1.69 | 12.6 | 23.04 | 0.712 | 1.345 |
| 270 | -3 | 1.2931 | 1.006 | 1.747 | 13.51 | 23.77 | 0.709 | 1.403 |
| 280 | 7 | 1.2484 | 1.006 | 1.803 | 14.44 | 24.5 | 0.706 | 1.461 |
| 290 | 17 | 1.2073 | 1.006 | 1.857 | 15.38 | 25.2 | 0.703 | 1.52 |
| 300 | 27 | 1.1614 | 1.007 | 1.846 | 15.89 | 26.3 | 0.707 | 2.216 |
| 310 | 37 | 1.1233 | 1.007 | 1.962 | 17.46 | 26.37 | 0.701 | 1.64 |
| 320 | 47 | 1.0883 | 1.008 | 2.016 | 18.52 | 27.09 | 0.7 | 1.7 |
| 330 | 57 | 1.0561 | 1.008 | 2.068 | 19.58 | 27.81 | 0.7 | 1.756 |
| 340 | 67 | 1.0258 | 1.009 | 2.119 | 20.65 | 28.51 | 0.699 | 1.82 |
| 350 | 77 | 0.995 | 1.009 | 2.169 | 21.8 | 29.2 | 0.697 | 1.883 |
| 360 | 87 | 0.9699 | 1.01 | 2.218 | 22.86 | 29.89 | 0.695 | 1.945 |
| 370 | 97 | 0.9435 | 1.01 | 2.266 | 24.02 | 30.57 | 0.694 | 2.006 |
| 380 | 107 | 0.9181 | 1.012 | 2.314 | 25.19 | 31.25 | 0.692 | 2.074 |
| 390 | 117 | 0.8937 | 1.013 | 2.362 | 26.43 | 31.92 | 0.69 | 2.138 |
| 400 | 127 | 0.8711 | 1.014 | 2.408 | 27.64 | 32.58 | 0.689 | 2.206 |
| 420 | 147 | 0.8301 | 1.017 | 2.499 | 30.1 | 33.9 | 0.687 | 2.337 |
| 440 | 167 | 0.7922 | 1.019 | 2.588 | 32.66 | 35.2 | 0.686 | 2.47 |
| 460 | 187 | 0.7571 | 1.021 | 2.675 | 35.32 | 36.48 | 0.685 | 2.605 |
| 480 | 207 | 0.724 | 1.024 | 2.76 | 38.13 | 37.74 | 0.684 | 2.742 |
| 500 | 227 | 0.6938 | 1.03 | 2.841 | 40.95 | 38.99 | 0.683 | 2.883 |
| 550 | 277 | 0.6307 | 1.04 | 3.043 | 48.23 | 41.91 | 0.68 | 3.244 |
| 600 | 327 | 0.5778 | 1.051 | 3.232 | 55.93 | 44.74 | 0.68 | 3.609 |
| 650 | 377 | 0.5332 | 1.063 | 3.415 | 64.06 | 47.48 | 0.682 | 4.014 |
| 700 | 427 | 0.4934 | 1.075 | 3.591 | 72.81 | 50.16 | 0.684 | 4.417 |
| 750 | 477 | 0.46 | 1.087 | 3.763 | 81.81 | 52.75 | 0.687 | 4.832 |
| 800 | 527 | 0.4305 | 1.099 | 3.928 | 91.26 | 55.29 | 0.69 | 5.275 |
| 850 | 577 | 0.4045 | 1.11 | 4.09 | 101.1 | 57.73 | 0.693 | 5.725 |
| 900 | 627 | 0.3817 | 1.121 | 4.25 | 111.3 | 60.12 | 0.696 | 6.179 |
| 950 | 677 | 0.3611 | 1.131 | 4.404 | 121.9 | 62.47 | 0.699 | 6.659 |
| 1000 | 727 | 0.3432 | 1.141 | 4.56 | 132.9 | 64.73 | 0.702 | 7.122 |
| 1100 | 827 | 0.3116 | 1.159 | 4.857 | 155.8 | 69.17 | 0.708 | 8.116 |
| 1200 | 927 | 0.2851 | 1.175 | 5.147 | 180.6 | 73.53 | 0.714 | 9.185 |
| 1300 | 1027 | 0.2628 | 1.189 | 5.426 | 206.5 | 77.92 | 0.72 | 10.18 |
| 1400 | 1127 | 0.2438 | 1.207 | 5.697 | 233.7 | 82.35 | 0.725 | 11.3 |
| 1500 | 1227 | 0.2278 | 1.225 | 5.961 | 261.7 | 86.88 | 0.728 | 12.35 |
| 1600 | 1327 | 0.2133 | 1.241 | 6.214 | 291.5 | 91.27 | 0.733 | 13.44 |
| 1800 | 1527 | 0.189 | 1.27 | 6.7 | 354.7 | 99.88 | 0.74 | 15.73 |
| 2000 | 1727 | 0.1706 | 1.296 | 7.16 | 419.8 | 108.4 | 0.745 | 18.06 |
Air Density ρ vs Temperature
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Formula Reference
Air Properties Table (1 atm) Formula
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When to Use This Calculator
- •Use the Air Properties Table (1 atm) when solving homework or exam problems that require quick numerical verification of your hand calculations — instant feedback helps identify arithmetic errors before they propagate.
- •Use it during the early design phase to rapidly iterate on parameters and narrow down feasible configurations before committing time to detailed finite element simulations or full design packages.
- •Use it when reviewing a colleague's calculation or checking a vendor's data sheet for plausibility — a quick sanity check can prevent costly downstream errors.
- •Use it to generate reference data for a technical report or presentation without manual computation, ensuring consistent, reproducible numbers throughout the document.
- •Use it in the field when a quick estimate is needed and a full engineering software package is not available.
About This Calculator
The Air Properties Table (1 atm) is a precision engineering calculation tool designed for students, engineers, and technical professionals. Temperature-dependent thermophysical properties of dry air: density, cp, viscosity, thermal conductivity, Prandtl number. 200K–2000K. Sortable. All calculations are performed using established engineering formulas from the relevant scientific literature and standards. Inputs support both metric (SI) and imperial unit systems, with unit conversion handled automatically — simply select your preferred unit from the dropdown next to each field. Results are computed instantly in the browser without sending data to a server, ensuring both speed and privacy. This calculator is intended as a supplementary tool for learning and design exploration; always verify results against authoritative references for safety-critical applications.
The Theory Behind It
Air properties tables tabulate the temperature-dependent thermophysical properties of dry air at 1 atm pressure across a wide temperature range (typically 200-2000 K). Key properties include density (ρ, kg/m³), specific heat at constant pressure (c_p, J/(kg·K)), dynamic viscosity (μ, Pa·s), kinematic viscosity (ν = μ/ρ, m²/s), thermal conductivity (k, W/(m·K)), thermal diffusivity (α, m²/s), and Prandtl number (Pr = ν/α = μc_p/k, dimensionless). These properties are used in convective heat transfer calculations, fluid mechanics analyses, and aerodynamic design. Air at standard conditions (15°C, 101.325 kPa) has density 1.225 kg/m³, viscosity 1.79 × 10⁻⁵ Pa·s, thermal conductivity 0.0253 W/(m·K), and Prandtl number approximately 0.715. As temperature increases, density decreases (ideal gas behavior), viscosity and thermal conductivity increase, and Prandtl number stays near 0.7. At high temperatures (above 1500 K), variable specific heat becomes significant and dissociation effects start to matter. At very low temperatures (below 200 K), condensation and departure from ideal gas behavior become important. The tables are essential for designing HVAC systems, combustion equipment, heat exchangers, gas turbines, and any application involving air as the working fluid or coolant.
Real-World Applications
- •HVAC system design: compute air density, viscosity, and thermal conductivity at design temperatures for duct sizing, fan selection, and heat exchanger calculations.
- •Gas turbine analysis: use temperature-dependent air properties for compressor and turbine efficiency calculations across the large temperature range from intake to turbine inlet.
- •Combustion equipment design: air properties are needed for computing combustion air flow, stoichiometric calculations, and exhaust gas heat transfer.
- •Aerodynamic analysis: compressibility corrections and boundary layer analysis require accurate air properties at flight conditions.
- •Electronic equipment cooling: natural and forced convection cooling of electronics uses air properties at component operating temperatures.
Frequently Asked Questions
What properties are in an air properties table?
Typically: temperature, density (ρ), specific heat (c_p), dynamic viscosity (μ), kinematic viscosity (ν), thermal conductivity (k), thermal diffusivity (α), and Prandtl number (Pr). Some tables also include ratio of specific heats (γ) and specific enthalpy. The tables assume dry air at 1 atm pressure; for other pressures, density scales with pressure (ideal gas) while transport properties (μ, k) are approximately pressure-independent.
What's Prandtl number for air?
For air at moderate temperatures, Pr ≈ 0.7-0.72, nearly constant across the 200-2000 K range. This means momentum diffuses slightly faster than thermal energy. Prandtl number is used in Nusselt number correlations for convective heat transfer and is one of the key dimensionless parameters in fluid mechanics and heat transfer calculations.
How does air density change with temperature?
For air at 1 atm (ideal gas): ρ = PM/(RT). At 300 K (27°C), ρ ≈ 1.177 kg/m³. At 1000 K (727°C), ρ ≈ 0.353 kg/m³. At 2000 K, ρ ≈ 0.176 kg/m³. Density decreases inversely with absolute temperature. For HVAC and combustion calculations, always use the density at the actual operating temperature, not standard conditions.
How much does air viscosity increase with temperature?
Air viscosity increases with temperature following Sutherland's formula or similar correlations. At 300 K: μ ≈ 1.85 × 10⁻⁵ Pa·s. At 1000 K: μ ≈ 4.25 × 10⁻⁵ Pa·s. At 2000 K: μ ≈ 6.93 × 10⁻⁵ Pa·s. This increase matters for high-temperature gas flow calculations and can significantly affect Reynolds number compared to using room-temperature viscosity.
Are these properties valid for humid air?
Standard tables assume dry air. For humid air, adjust using psychrometric relations — humid air has slightly lower density and different thermal properties than dry air. At typical HVAC conditions, the differences are a few percent and often negligible; for precision calculations or extreme conditions (high humidity or high temperature), use psychrometric-adjusted values.
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