A manometer is used to measure the air pressure in a tank. the fluid used has a specific gravity of 1.25, and the differential h
eight between the two arms of the manometer is 28 in. if the local atmospheric pressure is 12.7 psia, determine the absolute pressure in the tank for the cases of the manometer arm with the (a) higher and (b) lower fluid level being attached to the tank.
Specific Gravity of the fluid = 1.25 Height h = 28 in Atmospheric Pressure = 12.7 psia Density of water = 62.4 lbm/ft^3 at 32F Density of the Fluid = Specific Gravity of the fluid x Density of water = 1.25 x 62.4 Density of the Fluid p = 78 lbm/ft^3 Difference in pressure as we got the differential height, dP = p x g x h dP = (78 lbm/ft^3) x (32.174 ft/s^2) x (28/12 ft) [ 1 lbf / 32.174 ft/s^2] [1 ft^2 / 144in^2] Difference in pressure = 1.26 psia (a) Pressure in the arm that is at Higher P = Atmospheric Pressure - Pressure difference = 12.7 - 1.26 = 11.44 psia (b) Pressure in the tank that is at Lower P = Atmospheric Pressure + Pressure difference = 12.7 + 1.26 = 13.96psia
