Air Properties Table (1 atm)
Thermophysical properties of dry air at 1 atm from 200 K to 2000 K: density, cp, viscosity, thermal conductivity, Prandtl number and thermal diffusivity, generated with CoolProp. Sortable.
Thermophysical properties of dry air at 101.325 kPa from 200 K to 2000 K, computed with CoolProp. 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 | -73.15 | 1.7692 | 1.0068 | 1.3334 | 7.5366 | 18.503 | 0.72553 | 1.0388 |
| 220 | -53.15 | 1.6072 | 1.006 | 1.4443 | 8.9864 | 20.159 | 0.72073 | 1.2468 |
| 240 | -33.15 | 1.4725 | 1.0056 | 1.5515 | 10.537 | 21.773 | 0.71658 | 1.4704 |
| 250 | -23.15 | 1.4133 | 1.0055 | 1.6038 | 11.348 | 22.564 | 0.71471 | 1.5878 |
| 260 | -13.15 | 1.3587 | 1.0056 | 1.6553 | 12.183 | 23.346 | 0.71296 | 1.7088 |
| 270 | -3.15 | 1.3082 | 1.0056 | 1.706 | 13.041 | 24.119 | 0.71133 | 1.8333 |
| 280 | 6.85 | 1.2613 | 1.0058 | 1.756 | 13.922 | 24.883 | 0.7098 | 1.9614 |
| 290 | 16.85 | 1.2177 | 1.0061 | 1.8052 | 14.825 | 25.638 | 0.70838 | 2.0928 |
| 300 | 26.85 | 1.177 | 1.0064 | 1.8537 | 15.75 | 26.384 | 0.70706 | 2.2275 |
| 310 | 36.85 | 1.1389 | 1.0068 | 1.9016 | 16.696 | 27.123 | 0.70584 | 2.3654 |
| 320 | 46.85 | 1.1033 | 1.0073 | 1.9488 | 17.664 | 27.854 | 0.70472 | 2.5065 |
| 330 | 56.85 | 1.0698 | 1.0078 | 1.9954 | 18.652 | 28.578 | 0.70369 | 2.6507 |
| 340 | 66.85 | 1.0382 | 1.0085 | 2.0413 | 19.661 | 29.294 | 0.70275 | 2.7978 |
| 350 | 76.85 | 1.0085 | 1.0092 | 2.0867 | 20.691 | 30.003 | 0.7019 | 2.9478 |
| 360 | 86.85 | 0.98047 | 1.01 | 2.1315 | 21.74 | 30.706 | 0.70114 | 3.1007 |
| 370 | 96.85 | 0.95393 | 1.0109 | 2.1758 | 22.809 | 31.402 | 0.70046 | 3.2562 |
| 380 | 106.85 | 0.9288 | 1.0119 | 2.2196 | 23.897 | 32.092 | 0.69987 | 3.4145 |
| 390 | 116.85 | 0.90495 | 1.013 | 2.2628 | 25.005 | 32.775 | 0.69936 | 3.5753 |
| 400 | 126.85 | 0.88231 | 1.0141 | 2.3055 | 26.131 | 33.453 | 0.69893 | 3.7387 |
| 420 | 146.85 | 0.84026 | 1.0167 | 2.3896 | 28.439 | 34.792 | 0.6983 | 4.0726 |
| 440 | 166.85 | 0.80203 | 1.0196 | 2.4719 | 30.82 | 36.109 | 0.69796 | 4.4158 |
| 460 | 186.85 | 0.76714 | 1.0227 | 2.5525 | 33.273 | 37.406 | 0.69788 | 4.7677 |
| 480 | 206.85 | 0.73516 | 1.0262 | 2.6315 | 35.795 | 38.684 | 0.69805 | 5.1278 |
| 500 | 226.85 | 0.70574 | 1.0299 | 2.709 | 38.385 | 39.945 | 0.69845 | 5.4958 |
| 550 | 276.85 | 0.64157 | 1.04 | 2.8968 | 45.152 | 43.024 | 0.70026 | 6.4479 |
| 600 | 326.85 | 0.5881 | 1.0512 | 3.0769 | 52.319 | 46.011 | 0.70296 | 7.4427 |
| 650 | 376.85 | 0.54286 | 1.063 | 3.2502 | 59.872 | 48.919 | 0.70624 | 8.4775 |
| 700 | 426.85 | 0.50408 | 1.075 | 3.4176 | 67.798 | 51.755 | 0.70984 | 9.5512 |
| 750 | 476.85 | 0.47048 | 1.087 | 3.5796 | 76.085 | 54.53 | 0.71353 | 10.663 |
| 800 | 526.85 | 0.44108 | 1.0987 | 3.737 | 84.724 | 57.249 | 0.71718 | 11.813 |
| 850 | 576.85 | 0.41514 | 1.11 | 3.8901 | 93.707 | 59.918 | 0.72068 | 13.003 |
| 900 | 626.85 | 0.39208 | 1.1209 | 4.0394 | 103.03 | 62.543 | 0.72395 | 14.231 |
| 950 | 676.85 | 0.37145 | 1.1312 | 4.1853 | 112.67 | 65.128 | 0.72696 | 15.5 |
| 1000 | 726.85 | 0.35288 | 1.141 | 4.328 | 122.65 | 67.677 | 0.72967 | 16.809 |
| 1100 | 826.85 | 0.3208 | 1.1588 | 4.6052 | 143.55 | 72.68 | 0.73425 | 19.551 |
| 1200 | 926.85 | 0.29408 | 1.1745 | 4.8728 | 165.7 | 77.576 | 0.73774 | 22.46 |
| 1300 | 1026.85 | 0.27146 | 1.1882 | 5.1325 | 189.07 | 82.382 | 0.74029 | 25.54 |
| 1400 | 1126.85 | 0.25207 | 1.2003 | 5.3854 | 213.64 | 87.113 | 0.74206 | 28.791 |
| 1500 | 1226.85 | 0.23527 | 1.211 | 5.6325 | 239.41 | 91.782 | 0.74319 | 32.213 |
| 1600 | 1326.85 | 0.22057 | 1.2205 | 5.8748 | 266.35 | 96.398 | 0.74383 | 35.807 |
| 1800 | 1526.85 | 0.19607 | 1.2367 | 6.3471 | 323.72 | 105.5 | 0.74402 | 43.51 |
| 2000 | 1726.85 | 0.17646 | 1.2502 | 6.8068 | 385.74 | 114.49 | 0.74328 | 51.896 |
Air Density ρ vs Temperature
Tip: hover to read values, click to pin a point for export
Source: CoolProp 8.0.0. Density and c_p come from the air equation of state of Lemmon et al. (2000); viscosity and thermal conductivity from Lemmon & Jacobsen (2004). ν = μ/ρ, Pr = μc_p/k and α = k/(ρc_p) are computed from the same values, so the columns agree to rounding (five significant figures).
Validity: the air equation of state covers 60–2000 K, so the table stops at its 2000K limit. Lemmon & Jacobsen estimate uncertainties of about 1 % for the viscosity of dilute air above 200 K and 2–5 % for thermal conductivity, the larger figure at high temperatures. Air is modeled as a fixed, non-reacting mixture (no dissociation).
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When to Use This Calculator
- •Use the Air Properties Table (1 atm) to check your hand calculations on homework or exam problems — comparing its result with your own working 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. Thermophysical properties of dry air at 1 atm from 200 K to 2000 K: density, cp, viscosity, thermal conductivity, Prandtl number and thermal diffusivity, generated with CoolProp. Sortable. All calculations are performed using established engineering formulas from the relevant scientific literature and standards. Follow the units printed beside each field. Where a unit selector is provided, the selected unit is converted internally. Results are computed in your browser without sending data to a server, which keeps your inputs private. 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 1.2255 kg/m³, viscosity 1.80 × 10⁻⁵ Pa·s, thermal conductivity 0.0255 W/(m·K), and Prandtl number about 0.709. As temperature increases, density decreases (ideal gas behavior), viscosity and thermal conductivity increase, and the Prandtl number stays between about 0.70 and 0.74. Specific heat rises from 1.006 kJ/(kg·K) at 300 K to 1.141 at 1000 K and 1.250 at 2000 K. The table treats air as a fixed, non-reacting mixture (no dissociation). Below 200 K, outside this table, departures from ideal-gas behavior grow, and at 1 atm air condenses at about 79–82 K. 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 1 atm, Pr stays between about 0.70 and 0.74 from 200 K to 2000 K (0.707 at 300 K). 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 ≈ 4.33 × 10⁻⁵ Pa·s. At 2000 K: μ ≈ 6.81 × 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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References & Further Reading
Standards & Organizations
Academic Resources
- Viscosity and Thermal Conductivity Equations for Nitrogen, Oxygen, Argon, and Air (Lemmon & Jacobsen, 2004)International Journal of Thermophysics
Transport equations used for μ and k; the authors give uncertainties generally within 5 % for air, higher in the critical region.
Industry References
- CoolProp — open-source thermophysical property libraryCoolProp
Version 8.0.0 generated every value in this table.
Textbooks
- Lemmon, E. W., Jacobsen, R. T, Penoncello, S. G., Friend, D. G.. Thermodynamic Properties of Air and Mixtures of Nitrogen, Argon, and Oxygen From 60 to 2000 K at Pressures to 2000 MPa, J. Phys. Chem. Ref. Data 29(3), 331–385, 2000.
Equation of state for air used for density and c_p, valid from 60 K to 2000 K.
- Bell, I. H., Wronski, J., Quoilin, S., Lemort, V.. Pure and Pseudo-pure Fluid Thermophysical Property Evaluation and the Open-Source Thermophysical Property Library CoolProp, Ind. Eng. Chem. Res. 53(6), 2498–2508, 2014.
Describes the CoolProp library used to evaluate the equations.
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