Problem 4.1.2

 

Air is passing through 4-in ID pipe at 14.7 psi and 70 degrees Fahrenheit.  A manometer connected to the pitot tube measures a pressure drop of one inch of mercury.  What is the velocity of air?  Use pitot tube constant as 1.0.

 

Solution:

 

For manometers, pressure drop (delta P) is directly related to delta h.  If manometer fluid density is rho_m then, delta P is equal to delta h times rho_m minus rho times g over gc.  If height is measured in meter, density in kilogram per meter cubed, then delta P values is in pascals. 

 

Density of mercury is 13.56 gram per cc or 1.356 times 104 kilogram per cubic meter.  Density of air is 1.196 kilogram per cubic meter.  Pressure drop is calculated as 3.378 times 103 pascals.

 

If we consider that air is incompressible, then velocity of the fluid passing though the pipe is given by C time square root of 2 gc delta P over rho, where C is the ‘Pitot Tube Constant”.   Rho is the density of the fluid (air) that is passing though pipe.  Velocity is calculated as 75.148 meter per second.

 

Outlet pressure is found as 9.795 times 104 pascals.  For gases with adiabatic flow conditions, velocity is given as 74.69 meters per second.

Note that Pi is inlet pressure and Po is outlet pressure.

 

If the gas velocity is found greater than 200 feet per second, treat case as flow of compressible fluid.