Here h is the difference in the heights of the liquid columns in the manometer and pair and Piquid are the densities of air and the manometer liquid, respectively. At B, however, the speed of the air presumably equals the airspeed of the aircraft manometrud density Beginning with the principle of Conservation of Energy for a fluid (Bernoulli's Law), derive the expression VE 2 Pliquidgh Pair or the airspeed of a plane, v, on which a Pitot tube is mounted. A Pitot tube or similar velocity-measuring device consists. At the front opening, A, which points in the direction the plane is headed, the streamlines separate and there is a stagnation point where the air is not moving relative to the aircraft (that is, the fluid rushes away from the point A in all directions and the speed there is zero). discussions of velocity-measuring probes for the normal use of the engineer. The other arm of the manometer is connected to a hole, A, at the front end of the device. The device was commonly used Pitot Static Tube Total pressure on aircraft, where it was mounted on either the wing or fuselage to measure the speed of Pitot-Static Tube fud density constant another fluid (air) relative to the aircraft Fluid Row A Velocity C B CO A Pitot tube consists of an outer Pitot Tube tube with of small holes, B, that is connected to one arm of a U- Static tube tube or manometer.
The velocity of flow is Take coefficient of velocity as 0.98a)4.34 m/sb)5 m/sc)5.34 m/sd)6.47 m/sCorrect answer is option 'A'. The stagnation pressure head is 6 m and static pressure head is 5 m. His first application was B to measure the water speed of the Seine River in Paris in 1730. Apr 23,2022 - A pitot-static tube is used to measure the velocity of water in a pipe. Transcribed image text: Flow of meubleThuid VA Prese Vet Prere Traducer Statie pressure Henri Pitot was the first to use a simple device shown at right, now known as a Pitot or Prandul tube, to measure the speed of a De fluid.
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