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  2. File:Pitot tube types.svg - Wikipedia

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

    Download QR code; In other projects ... Types of pitot tubes. Examples of pitot tube, static tube, and pitot-static tube.

  3. File:Tube de Pitot, description.png - Wikipedia

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

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  4. 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 ...

  5. File:Pitot tube manometer.svg - Wikipedia

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

    You are free: to share – to copy, distribute and transmit the work; to remix – to adapt the work; Under the following conditions: attribution – You must give appropriate credit, provide a link to the license, and indicate if changes were made.

  6. Pitot–static system - Wikipedia

    en.wikipedia.org/wiki/Pitot–static_system

    Examples of pitot tube, static tube, and pitot–static tube Static ports fitted to an Airbus A330 passenger airliner. The pitot–static system of instruments uses the principle of air pressure gradient. It works by measuring pressures or pressure differences and using these values to assess the speed and altitude. [1]

  7. Thermodynamic diagrams - Wikipedia

    en.wikipedia.org/wiki/Thermodynamic_diagrams

    The main feature of thermodynamic diagrams is the equivalence between the area in the diagram and energy. When air changes pressure and temperature during a process and prescribes a closed curve within the diagram the area enclosed by this curve is proportional to the energy which has been gained or released by the air.

  8. Position error - Wikipedia

    en.wikipedia.org/wiki/Position_error

    The pitot tube supplies pressure to the airspeed indicator. Pitot pressure is equal to stagnation pressure providing the pitot tube is aligned with the local airflow, it is located outside the boundary layer, and outside the wash from the propeller.

  9. Rayleigh flow - Wikipedia

    en.wikipedia.org/wiki/Rayleigh_flow

    Therefore, the Rayleigh flow model is critical for an initial design of the duct geometry and combustion temperature for an engine. The Rayleigh flow model is also used extensively with the Fanno flow model. These two models intersect at points on the enthalpy-entropy and Mach number-entropy diagrams, which is meaningful for many applications.