Altitude is calculated on the basis of static air pressure and airspeeds are calculated on the difference between the static air pressure and pitot air pressure, therefore if the pitot tube were block the only instrument which would be affected would be the airspeed indicator. Static pressure ports are usually located on the skin of the aircraft where they are flush and cannot be affected by wind speed. ADDITIONAL INFO Static preasure is measured from the static port, usually located on the side of the aircraft. If the static port is blocked it usually freezes the altimeter at the last reading when the port was blocked. Many aircraft have a valve to switch to cabin preasure if the static port is blocked. Also you can break the glass of some altimeters so it will then use the cabin preasure to tell altitude. But beware that when you break the glass your vertical speed will read opposite, so it will say you are going up when you are going down etc. You can tell when the static port is blocked when the altitude reading doesn't change when the aircraft changes altitude.
One way to measure airspeed is to use a device called a pitot tube.
Instruments that measure wind speed include anemometers, which typically consist of rotating cups or blades that turn in the wind. The speed of rotation correlates to the wind speed, providing a measurable output. Another device is the pitot tube, which measures the difference in air pressure created by the wind, allowing for wind speed calculations. Additionally, handheld wind meters are used for portable measurements in various settings.
HA! That happened to me last month! An ANT got into the pitot tube and blocked the air flow. You have something keeping the air inside the tube. This is common with ice buildup on the tube. An AN=NT was a new one for me!
On most (all) modern aircraft there is more than 1 static port. In case the static ports are blocked, most pitot probes also have a static pressure sensor that will sense the pressure. (Tiny hole on the top or bottom of the probe) Static ports are one of the most important parts on an aircraft which is why you will always find an auxillary port for both pilots.
blocked pitot tube blocked static port density error compressibility error position errors
The pitot system provides impact pressure for the airspeed indicator instrument in an aircraft. This pressure measurement helps determine the speed of the aircraft relative to the surrounding air.
On such a system, you get to have 2 sets of "holes". One on the side of the aircraft, independent of the air flow, that measures the present atmospheric pressure. Comparing this pressure (static) with the ground one (given by the Airport Tower for a given area), gives you your altitude. The second "hole" (or set of holes) is in the front of the aircraft (usually the nose or close to the cockpit) and it has a membrane inside a tube that is pressed by the increased airflow created by the aircraft's speed. Comparing this pressure (pitot-tube pressure), with the fore-mentioned static one, gives you the aircraft's speed.
The Bernoulli equation is used to explain the relationship between fluid pressure, velocity, and elevation in a flowing fluid. In the context of a pitot tube, the Bernoulli equation helps to calculate the airspeed of an aircraft by comparing the total pressure and static pressure measured by the pitot tube. The pitot tube uses this principle to determine the speed of the aircraft based on the difference in pressure between the total pressure and static pressure.
One way to measure airspeed is to use a device called a pitot tube.
WingsTailLeading edgesSlatsProbes (Pitot, TAT, AOA etc)Antennae
The pitot (peetoe) tube is a device that has a small hole in the front that allows ram air pressure to go to the airspeed indicator. Under conditions with a lot of moisture in the air, especially in fog or in clouds or in precipitation, moisture can collect in the opening and freeze, thus blocking the pitot tube and cutting off your airspeed indication (or making it wrong, which is worse). The pitot heater prevents freezing. Pilots simply control this by flipping a switch in the cockpit of the aircraft, usually located near the Anti-icing switches for the aircraft.
James Pitot was born in 1761.
James Pitot died in 1831.
the airspeed indicator works by measuring the increase in air pressure caused by the moving aircraft