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pitot-static airspeed indicator

См. также в других словарях:

  • Pitot-static 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… …   Wikipedia

  • Airspeed indicator — The airspeed indicator or airspeed gauge is an instrument used in an aircraft to display the craft s airspeed, typically in knots, to the pilot. Markings Light aircraft Airspeed indicator markings use a set of standardized colored bands and lines …   Wikipedia

  • Pitot-static tube — noun measuring instrument consisting of a combined Pitot tube and static tube that measures total and static pressure; used in aircraft to measure airspeed • Syn: ↑Pitot head, ↑Pitot tube • Hypernyms: ↑measuring instrument, ↑measuring system,… …   Useful english dictionary

  • airspeed indicator — Aeron. a flight instrument showing the airspeed of an aircraft. Abbr.: ASI * * * ▪ instrument       instrument that measures the speed of an aircraft relative to the surrounding air, using the differential between the pressure of still air… …   Universalium

  • Airspeed — is the speed of an aircraft relative to the air. There are several different measures of airspeed: indicated airspeed, calibrated airspeed, equivalent airspeed and true airspeed.It is measured within the flying aircraft with an airspeed indicator …   Wikipedia

  • airspeed indicator — An instrument which displays the indicated airspeed of the aircraft derived from inputs of pitot and static pressures …   Military dictionary

  • Pitot tube — A Pitot (pronEng|ˈpiːtoʊ) tube is a pressure measurement instrument used to measure fluid flow velocity. The Pitot tube was invented by Italian born French engineer Henri Pitot in the early 1700s, and was modified to its modern form in the mid… …   Wikipedia

  • Static pressure — * In the design and operation of aircraft, static pressure is the air pressure in the aircraft’s static pressure system.* In fluid dynamics, static pressure is the pressure at a nominated point in a fluid. Many authors use the term static… …   Wikipedia

  • Calibrated airspeed — (CAS) is the speed shown by a conventional airspeed indicator after correction for instrument error and position error. Most EFIS diplays also show CAS. At high speeds and altitudes, calibrated airspeed is further corrected for compressibility… …   Wikipedia

  • Course Deviation Indicator — (CDI) is an avionics instrument used in aircraft navigation to determine an aircraft s lateral position in relation to a track. If the location of the aircraft is to the left of course, the needle deflects to the right, and vice versa. Contents 1 …   Wikipedia

  • True airspeed — (TAS) is the speed of an aircraft relative to the airmass in which it flies, i.e. the magnitude of the vector difference of the velocity of the aircraft and the velocity of the air. Under zero wind conditions and in horizontal flight, this is… …   Wikipedia

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