DRAG RACING CALCULATOR

Density Altitude
Calculator

Estimate moist-air density and corresponding standard-atmosphere altitude from measured station pressure, temperature and relative humidity.

Your setup

°F
Range: -40.00–140 °F
inHg
Use measured absolute station pressure, not sea-level-corrected weather pressure or altimeter setting.
%
Range: 0.00–100 %

Your results

Calculated
Estimated density altitude1,361.63ft
Moist-air density1.18kg/m³
Relative density96.08% ISA sea level

Density altitude is the altitude in a reference atmosphere with equal air density; it is not your measured elevation.

READ THE ASSUMPTIONS

Ideal-gas moist-air model within the stated input bounds and tropospheric approximation. Not for aviation navigation or engine-control calibration.

THE FORMULA

How the calculation works

Follow the formula and keep the input units consistent at every step.

e = RH/100 × 6.1078 × 10^(7.5T/(237.3+T)); ρ = (P−e)100/(287.05Tk) + e100/(461.495Tk); h = 44330.77[1−(ρ/1.225)^(1/4.25588)]
  1. Measure temperature in °C, absolute station pressure in hPa and relative humidity.
  2. Calculate water-vapor partial pressure and ideal moist-air density in kg/m³.
  3. Invert standard tropospheric density to estimate equivalent altitude in meters.

A Worked Example

Dry air at 15°C and 1013.25 hPa has density approximately 1.225 kg/m³ and density altitude approximately 0 m. Humidity lowers density at the same temperature and pressure.

What Your Result Means

Density altitude is the altitude in a reference atmosphere with equal air density; it is not your measured elevation.

Assumptions & Limitations

Ideal-gas moist-air model within the stated input bounds and tropospheric approximation. Not for aviation navigation or engine-control calibration.

Common Mistakes

Sea-level-corrected pressure can seriously understate density altitude at an elevated track.

QUICK ANSWERS

Questions about this calculation

Which values should I enter?

Measure temperature in °C, absolute station pressure in hPa and relative humidity. Sea-level-corrected pressure can seriously understate density altitude at an elevated track.

How should I interpret the result’s precision?

Displayed results are rounded for readability. Intermediate calculations retain floating-point precision; extra displayed decimals do not improve your input accuracy.

Can I use metric units?

Yes. Select Metric above the calculator to convert your inputs. Results always state their units. Tire-size designations keep their conventional mm and inch units.

What are the main limitations?

Ideal-gas moist-air model within the stated input bounds and tropospheric approximation. Not for aviation navigation or engine-control calibration.

Method, sources & relevant guides

Vapor pressure and virtual-temperature method. We calculate ideal moist-air density and invert standard tropospheric density; small rounding differences from the NWS implementation are expected.

NOAA / National Weather Service — Density altitude equations

Method documentation updated October 18, 2026. Independent professional review has not been claimed. Read the calculation and review policy.