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?
Automotive Technology: A Systems Approach (MindTap Course List)
6th Edition
ISBN:9781133612315
Author:Jack Erjavec, Rob Thompson
Publisher:Jack Erjavec, Rob Thompson
Chapter9: Automotive Engine Designs And Diagnosis
Section: Chapter Questions
Problem 13RQ: The stroke of an engine is the crank throw half twice four times equal to
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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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