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Omnikalc

Air density calculator from temperature, pressure and humidity

Calculate the density of air from temperature, barometric pressure and relative humidity, with density altitude for pilots and the effect on engines and sports.

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Results

Air density

1.2249 kg/m³

Density altitude

2 ft

In pounds per cubic foot
0.07647 lb/ft³
Compared with standard air (1.225 kg/m³)
100.0%

Why air density matters

The mass of air in a given volume determines how much lift a wing produces, how much power an engine makes, how far a baseball flies and how much drag a cyclist faces. It changes with temperature, pressure and humidity.

The formula

The calculator treats air as a mixture of dry air and water vapor:

  1. Saturation vapor pressure (Tetens): Es = 6.1078 × 10^(7.5 T ÷ (T + 237.3)) hPa.
  2. Actual vapor pressure: Pv = RH × Es.
  3. Density: ρ = (P − Pv) ÷ (287.058 × Tk) + Pv ÷ (461.495 × Tk), with pressures in pascals and Tk in kelvin.
  4. Density altitude: DA = 44,330.8 × (1 − (ρ ÷ 1.225)^0.234969) meters.

Worked example

At the standard sea-level conditions of 59 °F (15 °C), 29.92 inHg (1,013.25 hPa) and dry air, the density is 1.225 kg/m³ (0.0765 lb/ft³), 100% of standard, and the density altitude is zero.

Now take a summer afternoon in Denver: 90 °F, station pressure 24.9 inHg, 30% humidity. The density drops to about 0.96 kg/m³, only 78% of standard, and the density altitude climbs above 8,200 ft.

Effect of each factor

Change Effect on density
+10 °F (5.6 °C) about −2%
−1 inHg (−34 hPa) about −3.4%
From 0% to 100% humidity at 86 °F about −1.5%
+1,000 ft of elevation about −3%

Humid air is lighter, not heavier, because water molecules are lighter than the nitrogen and oxygen they displace.

Density altitude for pilots

Aircraft performance depends on density altitude, not on the elevation printed on the chart. Every 1,000 ft of density altitude above sea level reduces engine power by roughly 3% for a normally aspirated engine and lengthens the takeoff roll. “High, hot and humid” days are the classic trap at mountain airports.

Other uses

  • Baseball: a fly ball travels a few percent farther in thin air, one reason Coors Field in Denver is known as a hitter’s park.
  • Cycling and running: lower density means less aerodynamic drag, which is why hour records are often attempted at altitude.
  • HVAC and engines: fan airflow, combustion air and turbocharger maps are all corrected for density.

Which pressure to enter

Use the actual pressure at your location (station pressure). Weather reports usually give the altimeter setting or sea-level pressure, which is corrected to sea level and would overstate the density at altitude. The boiling point at altitude calculator can estimate the station pressure from your elevation.

Frequently asked questions

What is the density of air at sea level?

In the standard atmosphere, 1.225 kg/m³ or 0.0765 lb/ft³ at 59 °F (15 °C) and 29.92 inHg (1013.25 hPa) in dry air.

Does humid air weigh more than dry air?

No, it is lighter. Water vapor molecules (18 g/mol) are lighter than the nitrogen and oxygen they replace (about 29 g/mol), so humid air is slightly less dense at the same temperature and pressure.

What is density altitude?

The altitude in the standard atmosphere that has the same air density. On a hot day, an airport at 5,000 ft can have a density altitude above 8,000 ft, which lengthens the takeoff run and reduces climb performance.

Which pressure should I enter?

The actual station pressure where you are, not the sea-level corrected value given in weather reports. If you only have the sea-level value, use the boiling point at altitude calculator to estimate the station pressure from your elevation.

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Results are estimates provided for information purposes. They do not replace professional advice.