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Measurement of Atmospheric Pressure and Altitude

Accurate measurement of atmospheric pressure is essential for weather forecasting, altitude determination, and aircraft performance calculations. Pilots rely on pressure information to set flight instruments correctly and to evaluate how atmospheric conditions may affect flight operations.

Measurement of Atmospheric Pressure

Atmospheric pressure historically was measured in inches of mercury ("Hg) by a mercurial barometer. [Figure 1]

Although mercurial barometers are no longer used in the U. S., they are still a good historical reference for where the altimeter setting came from (inches of mercury)
Figure 1. Although mercurial barometers are no longer used in the U. S., they are still a good historical reference for where the altimeter setting came from (inches of mercury)

The barometer measures the height of a column of mercury inside a glass tube. A section of the mercury is exposed to the pressure of the atmosphere, which exerts a force on the mercury. An increase in pressure forces the mercury to rise inside the tube. When the pressure drops, mercury drains out of the tube decreasing the height of the column. This type of barometer is typically used in laboratories and weather observation stations, is not easily transported, and can be difficult to read.

An aneroid barometer is the standard instrument used to measure pressure; it is easier to read and transport. [Figure 2]

Aneroid barometer
Figure 2. Aneroid barometer

The aneroid barometer contains a closed vessel called an aneroid cell that contracts or expands with changes in pressure. The aneroid cell attaches to a pressure indicator with a mechanical linkage to provide pressure readings. The pressure sensing part of an aircraft altimeter is essentially an aneroid barometer. It is important to note that due to the linkage mechanism of an aneroid barometer, it is not as accurate as a mercurial barometer.

To provide a common reference, the International Standard Atmosphere (ISA) has been established. These standard conditions are the basis for certain flight instruments and most aircraft performance data. Standard sea level pressure is defined as 29.92 inHg, and standard sea level temperature is 59 °F (15 °C). Atmospheric pressure is also reported in millibars (mb), with 1 inHg equal to approximately 33.86 mb. Standard sea level pressure is 1,013.2 mb. Typical mb pressure readings range from 950.0 to 1,040.0 mb. Surface charts, high and low pressure centers, and hurricane data are reported using mb.

Since weather stations are located around the globe, all local barometric pressure readings are converted to a sea level pressure to provide a standard for records and reports. To achieve this, each station applies a correction factor based on its elevation and current atmospheric conditions to determine sea level pressure. For example, a station at 5,000 feet above sea level, with a reading of 24.92 inHg, reports a sea level pressure reading of 29.92 inHg. [Figure 3]

Station pressure is converted to and reported in sea level pressure
Figure 3. Station pressure is converted to and reported in sea level pressure

Using common sea level pressure readings helps ensure aircraft altimeters are set correctly, based on the current pressure readings.

By tracking barometric pressure trends across a large area, weather forecasters can more accurately predict the movement of pressure systems and the associated weather. For example, tracking a pattern of rising pressure at a single weather station generally indicates the approach of fair weather. Conversely, decreasing or rapidly falling pressure usually indicates approaching bad weather and, possibly, severe storms.

Altitude and Atmospheric Pressure

As altitude increases, atmospheric pressure decreases. On average, with every 1,000 feet of increase in altitude, the atmospheric pressure decreases approximately 1 inHg. As pressure decreases, the air becomes less dense, producing a higher density altitude. As pressure decreases, density altitude increases and has a pronounced effect on aircraft performance.

Differences in air density caused by temperature variations can result in pressure differences within the atmosphere. This, in turn, creates motion in the atmosphere, both vertically and horizontally, in the form of currents and wind. The atmosphere is almost constantly in motion as it strives to reach equilibrium. These never-ending air movements set up chain reactions that cause a continuing variety in the weather.

Quick Review: Atmospheric Pressure Measurement

How do mercurial and aneroid barometers differ in operation and accuracy?
A mercurial barometer measures pressure by balancing the weight of a mercury column against the atmosphere; it is highly accurate but bulky and mostly limited to labs. An aneroid barometer uses a sealed, flexible aneroid cell that expands or contracts with pressure changes. While the aneroid design is portable and serves as the core mechanism inside aircraft altimeters, its mechanical linkage makes it slightly less accurate than a mercurial barometer.
Why and how do global weather stations convert local barometric pressure to sea level pressure?
Because weather stations exist at vastly different elevations, their raw pressure readings cannot be directly compared. To create a standard baseline for weather charts and altimeter settings, each station applies a correction factor based on its elevation to calculate what the pressure would be at mean sea level. For example, a station located at 5,000 feet elevation will add approximately 5.00 "Hg to its local reading to report its standard sea level pressure.
What is the standard pressure lapse rate and how does it influence density altitude?
Atmospheric pressure decreases at an average standard lapse rate of approximately 1 "Hg per 1,000 feet of altitude gain. As an aircraft climbs and ambient pressure drops, the air molecules spread out and become less dense. This reduction in pressure directly causes an increase in density altitude, which significantly degrades overall engine thrust and aerodynamic lift performance.