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Dry Air Properties at Temperatures and Pressures

Thermodynamic and transport properties of dry air at varying temperature and pressure.

dryairpropertiesData Table

Overview

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Thermodynamic and transport properties of dry air at atmospheric pressure (1 atm / 101.325 kPa) as a function of absolute temperature. Data span 175 K to 1900 K and cover specific heats, viscosity, thermal conductivity, Prandtl number, kinematic viscosity, density, and thermal diffusivity. Dry air is treated as an ideal gas mixture (approximately 78% N₂, 21% O₂, 1% Ar by volume) with a specific gas constant of 287.058 J/(kg·K).

The original source describes thermal conductivity as a measure of how quickly a material can absorb heat from its surroundings, and presents dry-air properties at one atmosphere from 175 K to 1900 K. It also calls out related viscosity references: Air - Absolute and Kinematic Viscosity - SI & Imperial Units and Air - Absolute and Kinematic Viscosity - Imperial Units.

For the full table with ratio of specific heats, thermal conductivity, Prandtl number, kinematic viscosity, density and diffusivity, the original page notes: rotate the screen. The restored source table below preserves those columns in the migrated page.

Key Formulas

Ideal Gas Density

ρ=PRairT\rho = \frac{P}{R_{\text{air}} \cdot T}

Density of dry air from pressure and absolute temperature, where Rair=287.058  J/(kg⋅K)R_{\text{air}} = 287.058\;\text{J/(kg·K)}.

Enthalpy Change

Δh=cpΔT\Delta h = c_p \cdot \Delta T

Enthalpy change over a temperature interval, using the specific heat at constant pressure.

Specific Heat Ratio

k=cpcvk = \frac{c_p}{c_v}

Ratio of specific heats; approaches 1.4 at low temperatures and decreases with increasing temperature as internal energy modes activate.

Sutherland's Law for Viscosity

μ=μ0(TT0)1.5T0+ST+S\mu = \mu_0 \left(\frac{T}{T_0}\right)^{1.5} \frac{T_0 + S}{T + S}

Approximate dynamic viscosity of air, with reference viscosity μ0\mu_0 at temperature T0T_0 and Sutherland constant S110.4  KS \approx 110.4\;\text{K}.

Variables

SymbolDescriptionSI Unit
PPAbsolute pressurePa
TTAbsolute temperatureK
RairR_{\text{air}}Specific gas constant for dry air (287.058)J/(kg·K)
ρ\rhoDensitykg/m³
cpc_pSpecific heat at constant pressurekJ/(kg·K)
cvc_vSpecific heat at constant volumekJ/(kg·K)
kkRatio of specific heats (cp/cvc_p/c_v)
μ\muDynamic viscositykg/(m·s)
ν\nuKinematic viscosity (μ/ρ\mu/\rho)m²/s
λ\lambdaThermal conductivityW/(m·K)
Pr\text{Pr}Prandtl number

Dry Air Properties at 1 atm

13 rows
Dry air properties at 1 atm (101.325 kPa). Density and kinematic viscosity values at atmospheric pressure.
Temperature(K)
cp(kJ/(kg·K))
cv(kJ/(kg·K))
k (cp/cv)
Dynamic Viscosity μ(10⁻⁵ kg/(m·s))
Thermal Conductivity λ(10⁻⁵ kW/(m·K))
Prandtl Number
Kinematic Viscosity ν(10⁻⁵ m²/s)
Density ρ(kg/m³)
2001.00250.71541.4011.3291.8090.7360.7531.765
2501.00310.7161.4011.5992.2270.721.1321.412
3001.00490.71781.41.8462.6240.7071.5681.177
3501.00820.72111.3982.0753.0030.6972.0561.009
4001.01350.72641.3952.2863.3650.6882.5910.882
5001.02950.74241.3872.674.0410.683.7820.706
6001.05110.7641.3763.0174.6610.685.1280.588
7001.0750.78791.3643.3325.2360.6846.6070.504
8001.09870.81161.3543.6245.7740.698.2140.441
10001.14110.8541.3364.1536.7540.70211.760.353
12001.17460.88751.3234.6267.640.71115.730.294
15001.21120.92411.3115.2648.8310.72222.360.235
19001.2440.95691.36.00810.2330.7332.340.186

Source: engineeringtoolbox.com

Dry Air Density and Viscosity vs Temperature (1 atm)

Air Density Calculator

Use the ideal gas law to compute density at any pressure and temperature.

Dry Air Density (Ideal Gas)

Dry Air Density, Viscosity and Kinematic Viscosity

Dry Air Heat and Enthalpy Change

Restored Original Source Tables

The following tables are restored from the original source page to preserve the complete reference data.

Dry Air - Thermodynamic and Physical Properties

35 rows
Dry Air - Thermodynamic and Physical Properties
- cp - (kJ/kgK)
- cv - (kJ/kgK)
Specific Heat
Ratio of Specific Heats - k - ( cp/cv)
Dynamic Viscosity - μ - (10-5kg/m s)
Thermal Conductivity (10-5kW/m K)
Prandtl Number
Kinematic Viscosity1) - ν - ( 10-5m2/s)
Density1) - ρ - (kg/m3)
Thermal Diffusivity - α - (10-6 m2/s)
1751.00230.71521.4011.1821.5930.7440.5862.017
2001.00250.71541.4011.3291.8090.7360.7531.76510.23
2251.00270.71561.4011.4672.020.7280.9351.569
2501.00310.7161.4011.5992.2270.721.1321.41215.72
2751.00380.71671.4011.7252.4280.7131.3431.284
3001.00490.71781.41.8462.6240.7071.5681.17722.18
3251.00630.71921.41.9622.8160.7011.8071.086
3501.00820.72111.3982.0753.0030.6972.0561.00929.5
3751.01060.72351.3972.1813.1860.6922.3170.9413
4001.01350.72641.3952.2863.3650.6882.5910.882437.66
4501.02060.73351.3912.4853.710.6843.1680.7844
5001.02950.74241.3872.674.0410.683.7820.706
5501.03980.75271.3812.8494.3570.684.4390.6418
6001.05110.7641.3763.0174.6610.685.1280.5883
6501.06290.77581.373.1784.9540.6825.8530.543
7001.0750.78791.3643.3325.2360.6846.6070.5043
7501.0870.79991.3593.4825.5090.6877.3990.4706
8001.09870.81161.3543.6245.7740.698.2140.4412
8501.11010.8231.3493.7636.030.6939.0610.4153
9001.12090.83381.3443.8976.2760.6969.9360.3922
9501.13130.84421.344.0266.520.69910.830.3716
10001.14110.8541.3364.1536.7540.70211.760.353
10501.15020.86311.3334.2766.9850.70412.720.3362
11001.15890.87181.3294.3967.2090.70713.70.3209
11501.1670.87991.3264.5117.4270.70914.70.3069
12001.17460.88751.3234.6267.640.71115.730.2941
12501.18170.89461.3214.7367.8490.71316.770.2824
13001.18840.90131.3194.8468.0540.71517.850.2715
13501.19460.90751.3164.9528.2530.71718.940.2615
14001.20050.91341.3145.0578.450.71920.060.2521
15001.21120.92411.3115.2648.8310.72222.360.2353
16001.22070.93361.3085.4579.1990.72424.740.2206
17001.22930.94221.3055.6469.5540.72627.20.2076
18001.2370.94991.3025.8299.8990.72829.720.1961
19001.2440.95691.36.00810.2330.7332.340.1858

Source: engineeringtoolbox.com

Engineering Notes

  • Pressure dependence. The tabulated values assume 1 atm. At elevated pressures, density scales linearly with pressure (ideal gas), but viscosity and thermal conductivity are nearly independent of pressure for moderate ranges.
  • Humidity effects. Moist air is less dense than dry air at the same temperature and pressure because water vapor (M = 18.015 g/mol) is lighter than the average air molecule (M ≈ 28.97 g/mol). Use humidity-corrected properties for HVAC and psychrometric calculations.
  • Specific heat increase. At low temperatures only translational and rotational modes contribute. Above ~500 K, vibrational modes progressively activate, raising both cpc_p and cvc_v and reducing the ratio kk.
  • Prandtl number plateau. For air, Pr stays in the narrow range 0.68–0.73 across the full temperature span, making it a convenient constant in many convective heat transfer correlations.
  • Kinematic viscosity. Values marked with superscript 1 in the source are at atmospheric pressure. Because ν=μ/ρ\nu = \mu/\rho, it increases strongly with temperature as density drops.
  • High-temperature dissociation. Above roughly 2000 K, O₂ and N₂ begin to dissociate and the ideal gas property tables become unreliable. Use thermochemical equilibrium codes for combustion and plasma applications.

References