Using Pitot-static tube to Determine Helium Velocity

How can we determine the velocity of helium in a pipe using a Pitot-static tube?

Given the temperature and pressure of 4°C and 172 KPa (abs) respectively, what is the velocity of helium and is the flow considered incompressible?

Determination of Helium Velocity

To determine the velocity of helium in the pipe using a Pitot-static tube, we can utilize the Bernoulli's equation. The equation states that the total pressure in a fluid flow is the sum of the static pressure and dynamic pressure.

Calculating Velocity

The static pressure is given as 172 KPa (abs), and the dynamic pressure can be calculated using the water manometer reading of 0.06 m. By converting this reading to pressure, we can then substitute both static and dynamic pressures into the Bernoulli's equation to solve for the helium velocity.

Consideration of Flow Compressibility

To determine if the flow of helium can be considered incompressible, we need to calculate the Mach number of the flow. If the Mach number is less than 0.3, the flow is deemed incompressible; otherwise, it is compressible.

A Pitot-static tube is a device commonly used in fluid mechanics to measure the velocity of fluid flow within a pipe. In this scenario, the Pitot-static tube is specifically employed to determine the velocity of helium flowing through a pipe. The given conditions include a temperature of 4°C and a pressure of 172 KPa (abs).

To calculate the velocity of helium, we first need to apply the Bernoulli's equation. This fundamental principle in fluid dynamics enables us to analyze the pressure variations in the fluid flow. By knowing the static pressure (172 KPa) and measuring the dynamic pressure using the water manometer (0.06 m), we can then plug these values into the Bernoulli's equation to solve for the velocity of helium.

Furthermore, in assessing the compressibility of the helium flow, we consider the Mach number. The Mach number, defined as the ratio of the flow velocity to the speed of sound, provides insights into the compressibility of the fluid flow. If the Mach number is less than 0.3, we can reasonably assume that the flow is incompressible. Otherwise, if the Mach number exceeds 0.3, the flow is considered compressible.

By employing these calculations and principles, we can accurately determine the velocity of helium in the pipe using the Pitot-static tube and make informed judgments regarding the compressibility of the flow.

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