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  2. Pitot tube - Wikipedia

    en.wikipedia.org/wiki/Pitot_tube

    This example, from an Airbus A380, combines a pitot tube (right) with a static port and an angle-of-attack vane (left). Air-flow is right to left. Types of pitot tubes A pitot-static tube connected to a manometer Pitot tube on Kamov Ka-26 helicopter A Formula One car during testing with frames holding many pitot tubes Location of pitot tubes on ...

  3. 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

  4. 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 ...

  5. 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 ...

  6. Stagnation pressure - Wikipedia

    en.wikipedia.org/wiki/Stagnation_Pressure

    The two points of interest are 1) in the freestream flow at relative speed where the pressure is called the "static" pressure, (for example well away from an airplane moving at speed ); and 2) at a "stagnation" point where the fluid is at rest with respect to the measuring apparatus (for example at the end of a pitot tube in an airplane).

  7. 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]

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

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

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  9. Air flow bench - Wikipedia

    en.wikipedia.org/wiki/Air_flow_bench

    There are several possible types of metering element in use. Flow benches ordinarily use one of three types: orifice plate, venturi meter and pitot/static tube, all of which deliver similar accuracy. Most commercial machines use orifice plates due to their simple construction and the ease of providing multiple flow ranges.