The water in a tank is pressurized by air, and the pressure is measured by a multifluid manometer as shown. The tank is located on a mountain at an altitude of 1400m where the atmospheric pressure is 89.6 kPa. Determine the pressure of air in the tank if h1 = 0.5m, h2 = 0.5m, and h3 = 0.6m. Take the densities of water, oil and mercury to be 1000kg/.850 kg/and 13,600 kg/ The water in a tank is pressurized by air, and the pressure is measured by a multifluidmanometer as shown. The tank is located on a mountain at an altitude of 1400mwhere the atmospheric pressure is 89.6 kPa. Determine the pressure of air in the tankif h = 0.5m, h2 = 0.5m, and h3 = 0.6m,. Take the densities of water, oil and mercury tobe 1000kg/, 850 kg/and 13,600 kg/OdAIRWATER

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The water in a tank is pressurized by air, and the pressure is measured by a multifluid manometer as shown. The tank is located on a mountain at an altitude of 1400m where the atmospheric pressure is 89.6 kPa. Determine the pressure of air in the tank if h 0.5m, h2 = 0.5m, and h3 =0.6m,. Take the densities of water, oil and mercury to be 1000kg/, 850 kg/and 13,600 kg/ %3D AIR WATER

The water in a tank is pressurized by air, and the pressure is measured by a multifluid manometer as shown. The tank is located on a mountain at an altitude of 1400m where the atmospheric pressure is 89.6 kPa. Determine the pressure of air in the tank if h 0.5m, h2 = 0.5m, and h3 =0.6m,. Take the densities of water, oil and mercury to be 1000kg/, 850 kg/and 13,600 kg/ %3D AIR WATER

Structural Analysis

6th Edition

ISBN:9781337630931

Author:KASSIMALI, Aslam.

Publisher:KASSIMALI, Aslam.

Chapter2: Loads On Structures

Section: Chapter Questions

Problem 1P

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