Engine Tuner's Calculator
- using selectable units and dew point -
Air Temperature should ideally be the temperature of the air that is going into the intake of the engine.
Altimeter Setting is the value in the Kollsman window of an altimeter when it is set to correctly read the elevation. The altimeter setting is generally included in NOAA weather data reports. (For more information about ambient air pressure measurements see the pressure measurement page.)
Dew Point temperature is used in this calculator, rather than relative humidity, because the dew point is essentially constant for a given air mass. That is, the dew point changes rather slowly and is not significantly affected by temperature. On the other hand, the relative humidity changes greatly during the day as the air temperature changes.
Note: The altimeter setting and dew point can often be gathered from a local airport, local weather service or the national weather service. Click here for NOAA weather data including hourly listing of dew point and altimeter setting for worldwide locations, in both English and Metric units.
Altitude is the actual altitude at which the engine is being operated.
Relative Horsepower shows how air density alters the power output of a properly tuned engine. For example, at 85 deg F, 30.14 in-Hg altimeter setting, 58 deg F dew point and 5000 ft altitude, the engine only produces about 81.1% of the rated horsepower.
Note: The relative horsepower calculations are made in accordance with SAE J1349. The standard reference conditions for SAE J1349 are: Air temp 77 deg F (25 deg C), 29.235 Inches- Hg (990 mb) actual pressure and 0% relative humidity.
Note: Section 5.1 of SAE J1349 AUG2004 makes it clear that the equations are not intended to provide accurate corrections over an extremely wide range, but rather that the intended range of air temperatures is 15 to 35 deg C (59 to 95 deg F), and the intended range of dry air pressures is 900 to 1050 mb (26.58 to 31.01 inches-Hg). Values outside of this range may produce inaccurate results for SAE Relative Horsepower and Dyno Correction Factor, but all other calculator results (such as Density Altitude, Air Density, etc) will still be correct.
Dyno Correction Factor, also calculated according to SAE J1349 JUN90, is simply the reciprocal of the relative horsepower value.
Air Density is the actual weight of a given volume of air. This is a key parameter for engine tuning.
Air Density is the actual mass of a given volume of air. This is a key parameter for engine tuning.
Density Altitude is the altitude in dry air that would have the same density as the input conditions.
Note: The ICAO standard conditions for zero density altitude are 0 meters altitude, 15 deg C (59 deg F) air temp, 1013.25 mb (29.921 in-Hg) pressure and 0 % relative humidity.
Relative Air Density is the ratio of the calculated air density to the air density at sea level using the International Civil Aviation Organization (ICAO) standard reference conditions.
Note: The ICAO standard sea level air density is 1.225 kg/m3.
Virtual Temperature is the temperature of dry air which would have the same density as the input conditions.
Absolute Air Pressure is also called the station pressure and is the actual (uncorrected) ambient air pressure.
Note: For more information about ambient air pressure measurements see the pressure measurement page.
Vapor Pressure is the contribution of water vapor pressure to the total absolute air pressure.
Relative Humidity is the ratio of the water vapor pressure to the saturated vapor pressure.
Last Updated: 3-Apr-2012