Here, air (105 kPa) at 37 degrees celcius is flowing upward in a 6cm diamater inclined duct, at a rate of 90 L/s. In this case the density of air is 1.1 kg/m3. The diameter of the duct reduces to 4cm through a reducer and a pressure charge occurs. This pressure change is measured by a water manometer. The elevation difference between the points where the two arms of the manometer are attached is 0.2 meters. What is the differential height between the fluid levels in the two manometer arms?
Here, air (105 kPa) at 37 degrees celcius is flowing upward in a 6cm diamater inclined duct, at a rate of 90 L/s. In this case the density of air is 1.1 kg/m3. The diameter of the duct reduces to 4cm through a reducer and a pressure charge occurs. This pressure change is measured by a water manometer. The elevation difference between the points where the two arms of the manometer are attached is 0.2 meters. What is the differential height between the fluid levels in the two manometer arms?
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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Here, air (105 kPa) at 37 degrees celcius is flowing upward in a 6cm diamater inclined duct, at a rate of 90 L/s. In this case the density of air is 1.1 kg/m3. The diameter of the duct reduces to 4cm through a reducer and a pressure charge occurs. This pressure change is measured by a water manometer. The elevation difference between the points where the two arms of the manometer are attached is 0.2 meters. What is the differential height between the fluid levels in the two manometer arms?
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