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4. Determine the required cross-sectional areas of members BE, CD and CE of the given truss shown, if the allowable stress in tension is 120MPa while in compression is 105MPA. D G 4m 3m 3m B E F H 3m 3m 3m 3m 50KN 75KN 50KN

4. Determine the required cross-sectional areas of members BE, CD and CE of the given truss shown, if the allowable stress in tension is 120MPa while in compression is 105MPA. D G 4m 3m 3m B E F H 3m 3m 3m 3m 50KN 75KN 50KN

Structural Analysis
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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TNT VOLTE 044% 1:37 PROBLEM SET NO. 1_STRESS ANALYSIS_SIMPLE STRESS.pdf 4. Determine the required cross-sectional areas of members BE, CD and CE of the given truss shown, if the allowable stress in tension is 120MPA while in compression is 105MPA. G 4m 3m 3m E A 3m 3m 3m 3m 50KN 75KN 50KN ...
Transcribed Image Text:TNT VOLTE 044% 1:37 PROBLEM SET NO. 1_STRESS ANALYSIS_SIMPLE STRESS.pdf 4. Determine the required cross-sectional areas of members BE, CD and CE of the given truss shown, if the allowable stress in tension is 120MPA while in compression is 105MPA. G 4m 3m 3m E A 3m 3m 3m 3m 50KN 75KN 50KN ...
TNT VOLTE 044% 1:37 PROBLEM SET NO. 1_STRESS ANALYSIS_SIMPLE STRESS.pdf 1. As shown below, two pneumatic cylinders are used to control the motion and displacement of the device arm ABC. Assuming that the control rods attached at A and D each have a 20-mm diameter and happen to be parallel in the position shown. Solve for the average normal stress in (a) member AE, (b) member DG if the applied load at point C is 800 N. 150 mm 800 N 300 mm 600 mm- OB 400 mm 150 mm 200 mm
Transcribed Image Text:TNT VOLTE 044% 1:37 PROBLEM SET NO. 1_STRESS ANALYSIS_SIMPLE STRESS.pdf 1. As shown below, two pneumatic cylinders are used to control the motion and displacement of the device arm ABC. Assuming that the control rods attached at A and D each have a 20-mm diameter and happen to be parallel in the position shown. Solve for the average normal stress in (a) member AE, (b) member DG if the applied load at point C is 800 N. 150 mm 800 N 300 mm 600 mm- OB 400 mm 150 mm 200 mm
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