pitot-static tube Sentence Examples
- The pitot-static tube measures the airspeed of an aircraft by comparing the static pressure and the ram pressure.
- The pitot-static tube is composed of three main components: the pitot tube, the static tube, and the venturi tube.
- The pitot tube measures the ram pressure, which is the pressure exerted by the air as it flows into the pitot tube.
- The static tube measures the static pressure, which is the pressure exerted by the air at the side of the aircraft.
- The venturi tube creates a pressure difference between the pitot tube and the static tube, which is proportional to the airspeed.
- The pressure difference between the pitot tube and the static tube is measured by a diaphragm or a bellows.
- The output of the pitot-static tube is a voltage signal that is proportional to the airspeed.
- The pitot-static tube is a critical component of an aircraft's airspeed indicator.
- The pitot-static tube can also be used to measure the altitude and the angle of attack of an aircraft.
- Pitot-static tubes are also used in wind tunnels and other applications where it is necessary to measure airspeed or pressure.
pitot-static tube Meaning
pitot-static tube (n)
measuring instrument consisting of a combined Pitot tube and static tube that measures total and static pressure; used in aircraft to measure airspeed
Synonyms & Antonyms of pitot-static tube
No Synonyms and anytonyms found
FAQs About the word pitot-static tube
measuring instrument consisting of a combined Pitot tube and static tube that measures total and static pressure; used in aircraft to measure airspeed
No synonyms found.
No antonyms found.
The pitot-static tube measures the airspeed of an aircraft by comparing the static pressure and the ram pressure.
The pitot-static tube is composed of three main components: the pitot tube, the static tube, and the venturi tube.
The pitot tube measures the ram pressure, which is the pressure exerted by the air as it flows into the pitot tube.
The static tube measures the static pressure, which is the pressure exerted by the air at the side of the aircraft.
