Arduino Pitot Tube Wind Speed and Airspeed Indicator - Theory and Experiments — Maker Portal

A pitot tube, mounted on an airplane flying at 8000 m standard altitude, reads a stagnation pressure of 57 kPa. Estimate the plane's (a) velocity and (b) Mach number. | Numerade

The Differential Pressure Flow Measuring Principle (Pitot tube) on Make a GIF

An Introduction to Pitot Tubes and Probes

Pitot Tube Working Principle - By TheEngineeringConcepts.com

A pitot tube is used to determine the airspeed of an airplane.... | Filo

SOLVED:A Pitot tube is used to measure the supersonic flow of air in a conduit. When the Pitot tube is installed in the conduit, a normal shock forms just ahead of the location where stagnation measurements are taken. The stagnation pressure and stagnation temperature measured by the Pitot tube are 400 kPa and 250^∘ C, respectively. Just upstream of the normal shock caused by the Pitot tube, the pressure is measured as 80 kPa. Determine the Mach number and the velocity of the flow in the conduit

The Differential Pressure Flow Measuring Principle (Pitot tube)