Example 7: The figure below shows a complex manometer. Calculate: 1. The gauge pressure of the air in the tube (2943 N/m²). 2. The gauge pressure at A (20718.72 N/m²). 3. The absolute pressure at A if the atmospheric pressure is 105Nm-2 (120718.72 N/m²). S.g.= 0.90 s.g.= 2.94 B Air 0.3m D 0.8m t Water 0.6m (3 Density of water = 1000 kg/m³.

Example 7: The figure below shows a complex manometer. Calculate: 1. The gauge pressure of the air in the tube (2943 N/m²). 2. The gauge pressure at A (20718.72 N/m²). 3. The absolute pressure at A if the atmospheric pressure is 105Nm-2 (120718.72 N/m²). S.g.= 0.90 s.g.= 2.94 B Air 0.3m D 0.8m t Water 0.6m (3 Density of water = 1000 kg/m³.

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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