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TRY THIS ONE ON YOUR OWN!! Seatwork 1-M Figure: The composite member is shown in the figure. If the rigid bar remains horizontal after the loading is applied and a temperature change of +10°C. Determine the total stresses on each of the vertical members considering actual stress due to the loading carried and due to temperature change. Given on the table below are the properties of each material used as members. (steel) 500 mm 150 kN 150 mm 150 mm Steel Rigid Brass (rigid bar) 250 mm Area (mm2) 700 1500 E (GPa) (brass) 200 100 α (μm/mC) 11.7 17.6

TRY THIS ONE ON YOUR OWN!! Seatwork 1-M Figure: The composite member is shown in the figure. If the rigid bar remains horizontal after the loading is applied and a temperature change of +10°C. Determine the total stresses on each of the vertical members considering actual stress due to the loading carried and due to temperature change. Given on the table below are the properties of each material used as members. (steel) 500 mm 150 kN 150 mm 150 mm Steel Rigid Brass (rigid bar) 250 mm Area (mm2) 700 1500 E (GPa) (brass) 200 100 α (μm/mC) 11.7 17.6

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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TRY THIS ONE ON YOUR OWN! Seatwork 1-M Figure: The composite member is shown in the figure. If the rigid bar remains horizontal after the loading is applied and a temperature change of +10°C. Determine the total stresses on each of the vertical members considering actual stress due to the loading carried and due to temperature change. Given on the table below are the properties of each material used as members. (steel) 500 mm 150 kN 150 mm 150 mm Steel Rigid Brass (rigid bar) 250 mm Area (mm2) 700 1500 E (GPa) (brass) 200 100 --- a (um/meC) 11.7 17.6
Transcribed Image Text:TRY THIS ONE ON YOUR OWN! Seatwork 1-M Figure: The composite member is shown in the figure. If the rigid bar remains horizontal after the loading is applied and a temperature change of +10°C. Determine the total stresses on each of the vertical members considering actual stress due to the loading carried and due to temperature change. Given on the table below are the properties of each material used as members. (steel) 500 mm 150 kN 150 mm 150 mm Steel Rigid Brass (rigid bar) 250 mm Area (mm2) 700 1500 E (GPa) (brass) 200 100 --- a (um/meC) 11.7 17.6
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