Density Altitude Calculator

Density altitude for drag racing

A normally aspirated engine makes less power in thin air, so racers compare passes made on different days by the density altitude at the track. Heat and humidity push it up, and so does a falling barometer. This table holds the dew point at 60 F and shows two altimeter settings side by side.

Not for flight planning. Use your aircraft's POH or flight manual and an official weather briefing.

Open these numbers in the calculator and change them to match your own conditions.

Track elevation 500 ft, dew point 60 F (16 C).
TemperatureAltimeter 29.70 inHgAltimeter 30.10 inHg
60 F (16 C)1,182 ft725 ft
70 F (21 C)1,826 ft1,371 ft
80 F (27 C)2,456 ft2,003 ft
90 F (32 C)3,071 ft2,620 ft
100 F (38 C)3,673 ft3,223 ft

Many racing weather stations report station pressure rather than an altimeter setting. The calculator takes either one: pick station pressure under Pressure input and enter the track elevation.

How these figures are worked out

Each figure uses the National Weather Service method: station pressure from the altimeter setting and elevation, vapour pressure from the dew point, then virtual temperature and density altitude. The calculator runs the same code. Figures are rounded to the nearest foot and are estimates.

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