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  2. Pitot–static system - Wikipedia

    en.wikipedia.org/wiki/Pitotstatic_system

    A pitot–static system is a system of pressure-sensitive instruments that is most often used in aviation to determine an aircraft's airspeed, Mach number, altitude, and altitude trend. A pitot–static system generally consists of a pitot tube, a static port, and the pitot–static instruments. [1]

  3. Talk:Pitot–static system - Wikipedia

    en.wikipedia.org/wiki/Talk:Pitotstatic_system

    Pitot–static system has been listed as one of the Engineering and technology good articles under the good article criteria. If you can improve it further, ...

  4. Pitot tube - Wikipedia

    en.wikipedia.org/wiki/Pitot_tube

    A pitot-static system generally consists of a pitot tube, a static port, and the pitot-static instruments. [5] Errors in pitot-static system readings can be extremely dangerous as the information obtained from the pitot static system, such as airspeed, is potentially safety-critical. Several commercial airline incidents and accidents have been ...

  5. Trailing cone - Wikipedia

    en.wikipedia.org/wiki/Trailing_Cone

    It does this by giving an accurate measurement of the ambient atmospheric pressure (static pressure) well clear of the aircraft's fuselage. The trailing cone system trails at least one fuselage length behind the aircraft (SpaceAge Control) via a high-strength pressure tube. Static pressure is measured forward of the cone by several static ports.

  6. Impact pressure - Wikipedia

    en.wikipedia.org/wiki/Impact_pressure

    An air data computer with inputs of pitot and static pressures is able to provide a Mach number and, if static temperature is known, true airspeed. [citation needed] Some authors in the field of compressible flows use the term dynamic pressure or compressible dynamic pressure instead of impact pressure. [3] [4]

  7. Pitot tube static anemometer - Wikipedia

    en.wikipedia.org/?title=Pitot_tube_static...

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  8. Pitot pressure - Wikipedia

    en.wikipedia.org/wiki/Pitot_pressure

    Pitot pressure is the pressure that is measured by a Pitot tube, an open-ended tube connected to a pressure-measuring device. For subsonic flow, pitot pressure is equal to the stagnation pressure (or total pressure) of the flow, and hence the term pitot pressure is often used interchangeably with these other terms.

  9. Henri Pitot - Wikipedia

    en.wikipedia.org/wiki/Henri_Pitot

    Henri Pitot (French: [ɑ̃ʁi pito]; May 3, 1695 – December 27, 1771) was a French hydraulic engineer and the inventor of the pitot tube.. In a pitot tube, the height of the fluid column is proportional to the square of the velocity of the fluid at the depth of the inlet to the pitot tube.