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  2. File:Pitot tube types.svg - Wikipedia

    en.wikipedia.org/wiki/File:Pitot_tube_types.svg

    Printable version; Page information; Get shortened URL; Download QR code; In other projects ... Examples of pitot tube, static tube, and pitot-static tube. עברית

  3. Pitot tube - Wikipedia

    en.wikipedia.org/wiki/Pitot_tube

    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. [5]

  4. File:Faa pitot static system.JPG - Wikipedia

    en.wikipedia.org/wiki/File:Faa_pitot_static...

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  5. File:Pitot tube wings without txt.jpg - Wikipedia

    en.wikipedia.org/wiki/File:Pitot_tube_wings...

    Pitot_tube_wings_without_txt.jpg (203 × 204 pixels, file size: 12 KB, MIME type: image/jpeg) This is a file from the Wikimedia Commons . Information from its description page there is shown below.

  6. Airspeed indicator - Wikipedia

    en.wikipedia.org/wiki/Airspeed_indicator

    The pitot tube may become blocked, because of insects, dirt or failure to remove the pitot cover. A blockage will prevent ram air from entering the system. If the pitot opening is blocked, but the drain hole is open, the system pressure will drop to ambient pressure, and the ASI pointer will drop to a zero reading. If both the opening and drain ...

  7. Airspeed - Wikipedia

    en.wikipedia.org/wiki/Airspeed

    The measurement and indication of airspeed is ordinarily accomplished on board an aircraft by an airspeed indicator (ASI) connected to a pitot-static system. The pitot-static system comprises one or more pitot probes (or tubes) facing the on-coming air flow to measure pitot pressure (also called stagnation, total or ram pressure) and one or ...

  8. 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]

  9. Indicated airspeed - Wikipedia

    en.wikipedia.org/wiki/Indicated_airspeed

    Indicated airspeed measured by pitot-tube can be approximately expressed by the following equation delivered from Bernoulli's equation. () NOTE: The above equation applies only to conditions that can be treated as incompressible. Liquids are treated as incompressible under almost all conditions.