1. Refer to the table below. Find the atmospheric pressure at 2120 m.AtmosphericPressure (kPa)Air Density(kg/m³)Altitude (m)0 (sea level)101.3251.22550095.461.167100089.871.112150084.551.058200079.501.006250074.700.957300070.110.909350065.870.863400061.660.819450057.750.777500054.050.736600047.220.660700041.110.590800035.660.526900030.800.46710,00026.500.41311,00022.700.36512,00019.400.31213,00016.580.26614,00014.170.22815,00012.110.1952. Find the equation for the four linear sections of the moment diagram below.| 25 kips | 25 kips| 25 kipsCDEАВ6 ft1 ft 2 ft2 ftM, (Kip.ft)453025 4. Find the determinate of [A].32[4]= 2-3 -10-3 -10105. Use the Gauss Elimination Method to solve the following systems of equations.x+y+z = 62x+5y+z =15-3x+ y+5z = 14

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1. Refer to the table below. Find the atmospheric pressure at 2120 m. Atmospheric Pressure (kPa) Air Density (kg/m) Altitude (m) 0 (sea level) 101.325 1.225 500 95.46 1.167 1000 89.87 1.112 1500 84.55 1.058 1.006 0.957 2000 79.50 2500 74.70 3000 70.11 0.909 3500 65.87 0.863 4000 4500 61.66 0.819 57.75 0.777

1. Refer to the table below. Find the atmospheric pressure at 2120 m. Atmospheric Pressure (kPa) Air Density (kg/m) Altitude (m) 0 (sea level) 101.325 1.225 500 95.46 1.167 1000 89.87 1.112 1500 84.55 1.058 1.006 0.957 2000 79.50 2500 74.70 3000 70.11 0.909 3500 65.87 0.863 4000 4500 61.66 0.819 57.75 0.777

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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