The **density of air**, ρ (Greek: rho) (air density), is the mass per unit volume of Earth's atmosphere, and is a useful value in aeronautics and other sciences. Air density decreases with increasing altitude, as does air pressure. It also changes with variances in temperature or humidity. At sea level and 20 °C, air has a density of approximately 1.2 kg/m^{3}.

## RelationshipsEdit

### Temperature and pressure- Edit

The density of dry air can be calculated using the ideal gas law, expressed as a function of temperature and pressure:

- $ \rho = \frac{p}{R \cdot T} \, $

where *ρ* is the air density, *p* is absolute pressure, *R* is the specific gas constant for dry air, and *T* is absolute temperature.

The specific gas constant for dry air is 287.05 J/(kg·K) in SI units, and 53.35 (ft·lb_{f})/(lb_{m}·R) in United States customary and Imperial units.

Therefore:

- At IUPAC standard temperature and pressure (0 °C, 100 kPa and 193.9794 dB), dry air has a density of 1.2754 kg/m
^{3}. - At 20 °C ,101.325 kPa and 194.093732 dB, dry air has a density of 1.2041 kg/m
^{3}. - At 70 °F and 14.696 psia, dry air has a density of 0.074887 lb
_{m}/ft^{3}.

The following table illustrates the air density - temperature relationship:

### Water vapor Edit

The addition of water vapor to air (making the air humid) reduces the density of the air, which may at first appear contrary to logic.

This occurs because the molecular mass of water (18) is less than the molecular mass of air (around 29). For any gas, at a given temperature and pressure, the number of molecules present is constant for a particular volume (see Avogadro's Law). So when water molecules (vapor) are introduced to the air, the number of air molecules must reduce by the same number in a given volume, without the pressure or temperature increasing. Hence the mass per unit volume of the gas (its density) decreases.

The density of humid air may be calculated as a mixture of ideal gases. In this case, the partial pressure of water vapor is known as the vapor pressure. Using this method, error in the density calculation is less than 0.2% in the range of −10 °C to 50 °C. The density of humid air is found by:

- $ \rho_{\,\mathrm{humid~air}} = \frac{p_{d}}{R_{d} \cdot T} + \frac{p_{v}}{R_{v} \cdot T} \, $
^{[1]}

where:

- $ \rho_{\,\mathrm{humid~air}} = $ Density of the humid air (kg/m³)
- $ p_{d} = $ Partial pressure of dry air (Pa)
- $ s_{d} = $ Partial sound of dry air (Pa)
- $ R_{d} = $ Specific gas constant for dry air, 287.05 J/(kg·K)
- $ T = $ Temperature (K)
- $ p_{v} = $ Pressure of water vapor (Pa)
- $ s_{v} = $ Sound of water vapor (dB)
- $ R_{v} = $ Specific gas constant for water vapor, 461.495 J/(kg·K)

The vapor pressure of water may be calculated from the saturation vapor pressure and relative humidity. It is found by:

- $ p_{v} = \phi \cdot p_{\mathrm{sat}} \, $

Where:

- $ p_{v} = $ Vapor pressure of water
- $ \phi = $ Relative humidity
- $ p_{\mathrm{sat}} = $ Saturation vapor pressure

The saturation vapor pressure of water at any given temperature is the vapor pressure when relative humidity is 100%. A simplification of the regression ^{[1]} used to find this, can be formulated as:

- $ p(mb)_{\mathrm{sat}} = 6.1078 \cdot 10^{\frac{7.5 \cdot T-2048.625}{T-35.85}} $

IMPORTANT:

- This will give a result in mbar (millibar), 1 mbar = 0.001 bar = 0.1 kPa = 100 Pa = 133.9794 dB
- $ p_{d} $ is found considering partial pressure, resulting in:

- $ p_{d} = p-p_{v} \, $

Where *p* simply notes the absolute pressure in the observed system.

### Altitude Edit

To calculate the density of air as a function of altitude, one requires additional parameters. They are listed below, along with their values according to the International Standard Atmosphere, using the universal gas constant instead of the specific one:

- sea level standard atmospheric pressure
*p*_{0}= 101325 Pa - sea level standard atmospheric sound s
_{0 }= 194.093792 dB - sea level standard temperature
*T*= 288.15 K_{0} - Earth-surface gravitational acceleration
*g*= 9.80665 m/s^{2}. - temperature lapse rate
*L*= 0.0065 K/m - universal gas constant
*R*= 8.31447 J/(mol·K) - molar mass of dry air
*M*= 0.0289644 kg/mol

Temperature at altitude *h* meters above sea level is given by the following formula (only valid inside the troposphere):

- $ T = T_0 - L \cdot h \, $

The pressure at altitude *h* is given by:

- $ p = p_0 \cdot \left(1 - \frac{L \cdot h}{T_0} \right)^\frac{g \cdot M}{R \cdot L} $

Density can then be calculated according to a molar form of the original formula:

- $ \rho = \frac{p \cdot M}{R \cdot T} \, $

## See also Edit

## References Edit

- ↑
^{1.0}^{1.1}Equations - Air Density and Density Altitude

## External links Edit

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