# Airspeed Indicators

Airspeed Indicator :

The basic airspeed indicator on a Cessna 152 or an F-15E both read Indicated AirSpeed (IAS). Airspeed Indicators device measures the difference between Static pressure (usually from a sensor not in the airstream) and Impact pressure (called the stagnation pressure received from an aircraft’s Pitot Tube – which is in the airstream). When the aircraft is not moving, the pressures are equal (and the airspeed is zero). On takeoff, the on-rushing air will result in a greater pressure in the Pitot Tube and this difference in pressure from the static sensor can be used to calculate the airspeed (in miles per hour (MPH) or nautical miles per hours (KNOTS)) at which the aircraft is moving through the air.

The velocity is given by the square root of (2 x [stagnation pressure - static pressure] / air density).

The Airspeed Indicator is similar to a speedometer in a car. It shows the speed (in knots) of the airplane traveling through air. Here in the figure the speed is 110 knots (nautical miles per hour). A nautical mile is a measure of distance and is about 15% longer than a mile measured on land.

Types of Air Speed Indicator :

The airspeed indicator discussed above measures the aircraft’s speed through the air. At sea level, this speed is very close to the aircraft’s True Air Speed (TAS). TAS is the actual airspeed of the aircraft through the air mass. As an aircraft climbs, the indicated airspeed will decrease as the air becomes thinner and the impact pressure is reduced.

For example, at sea level a TAS of 440 MPH will equal an IAS of about 440. At 20,000 feet, a TAS of 440 MPH will have an IAS of about 360. Thus, for a given TAS, indicated airspeed will decrease with altitude.

True Airspeed adjusts the IAS for the given temperature and pressure. The F-15E receives TAS from the Air Data Computer which measures the outside temperature and pressure.

Ground Speed is another important airspeed to pilots. Ground speed is the aircraft’s actual speed across the earth. It equals the TAS plus or minus the wind factor. For example, if your TAS is 500 MPH and you have a direct (180 degrees from your heading) tail-wind of 100 MPH, your ground speed is 600 MPH.

Ground speed can be measured by onboard Inertial Navigation Systems (INS) or by Global Positioning Satellite (GPS) receivers. One “old-fashion” method is to record the time it takes to fly between two known points. Then divide this time by the distance. For example, if the distance is 18 miles, and it took an aircrew in an F-15E 2 minutes to fly between the points, then their groundspeed is :

1. 18 miles / 2 minutes = 9 miles per minute.
2. This can be converted to miles per hour by multiplying by 60 (60 minutes in an hour).
3. 9 miles per minute X 60 minutes per hour = 540 Miles per hour.